Patent Application
20250199158
Light detection and ranging (lidar) and radio detection and ranging (radar) are technologies that can be used to measure distances to remote targets. Typically, a lidar system includes a light source and an optical receiver and a radar system includes a radar frequency (RF) source and a radar receiver. The light source of a lidar system can include, for example, a laser which emits light having a particular operating wavelength. The operating wavelength of a lidar system may lie, for example, in the infrared, visible, or ultraviolet portions of the electromagnetic spectrum. The light source emits light towards a target which scatters the light, and some of the scattered light is received back at the lidar receiver. The lidar system determines the distance to the target based on one or more characteristics associated with the received light. For example, the lidar system may determine the distance to the target based on the time of flight for a pulse of light emitted by the light source to travel to the target and back to the lidar system. The RF source of a radar system emits RF signals towards a target which scatters the RF signals. Some of the scattered RF signals are received back at the radar receiver. The radar system determines the distance of a target based on reflected RF signals.
Various embodiments of the invention are disclosed in the following detailed description and the accompanying drawings.
The invention can be implemented in numerous ways, including as a process; an apparatus; a system; a composition of matter; a computer program product embodied on a computer readable storage medium; and/or a processor, such as a processor configured to execute instructions stored on and/or provided by a memory coupled to the processor. In this specification, these implementations, or any other form that the invention may take, may be referred to as techniques. In general, the order of the steps of disclosed processes may be altered within the scope of the invention. Unless stated otherwise, a component such as a processor or a memory described as being configured to perform a task may be implemented as a general component that is temporarily configured to perform the task at a given time or a specific component that is manufactured to perform the task. As used herein, the term ‘processor’ refers to one or more devices, circuits, and/or processing cores configured to process data, such as computer program instructions.
A detailed description of one or more embodiments of the invention is provided below along with accompanying figures that illustrate the principles of the invention. The invention is described in connection with such embodiments, but the invention is not limited to any embodiment. The scope of the invention is limited only by the claims and the invention encompasses numerous alternatives, modifications and equivalents. Numerous specific details are set forth in the following description in order to provide a thorough understanding of the invention. These details are provided for the purpose of example and the invention may be practiced according to the claims without some or all of these specific details. For the purpose of clarity, technical material that is known in the technical fields related to the invention has not been described in detail so that the invention is not unnecessarily obscured.
An integrated light detection and ranging (lidar) and radio detection and ranging (radar) system is disclosed. For example, using the disclosed integrated lidar and radar system, both light beams and radio frequency (RF) signals are emitted to scan one or more fields of regard. A scanned field of regard using light beams can be the same, different, or overlapping field of regard as the scanned field of regard using RF signals. In some embodiments, the different fields of regard overlap along one or more axes. For example, in the context of a vehicle equipped with the disclosed integrated lidar and radar system, the radar can be directed to scan downwards towards the road surface directly in front of the vehicle with a limited range in elevation while a corresponding lidar of the same integrated lidar and radar system can be directed to scan ahead of the vehicle with a large range in elevation that includes the horizon. As another example, the lidar can be directed to scan primarily ahead of the vehicle while the radar can be directed to scan regions that include the peripheries of the vehicle.
In some embodiments, the disclosed integrated lidar and radar system utilizes dual mode elements such as a shared processor and/or a dual mode scanner to allow for integrated detection and ranging using both light pulses and RF signals. For example, a shared processor can be used to process detected light pulse and RF signal reflections and to fuse the processed measurements. By processing lidar and radar measurements together in a synchronized and coupled manner, the processing can more easily and with reduced processing requirements address range wrap issues such as matching emitted light pulses with detected reflections. Additionally, the detection and ranging accuracy of the integrated system is significantly improved since both lidar and radar components can be operated with a higher tolerance to noise. For example, when operated in fog, radar can continue to penetrate through the fog even when lidar can be impacted by the fog due to increased noise such as back scatter from fog. When integrated together using the disclosed integrated lidar and radar system, the integrated radar can provide an initial view of the surrounding environment and function as a source of validation for results from the integrated lidar. The results from the integrated lidar, once validated with radar readings, can provide a more accurate scan of the environment than can be made with radar alone. The use of dual mode measurements from an integrated system allows signals that would otherwise be discarded as potential noise to be confirmed as accurate measurements corresponding to downrange objects.
In various embodiments, the coupled lidar and radar signals allow for processing of related signals earlier in the processing pipeline, resulting in significant improvements in the resulting measurements. The earlier correlation of related signals allowed by the disclosed inventions provides opportunities for refinement that allow for improved results such as increased resolution and higher accuracy, including with reduced processing power. For example, in scenarios where radar excels, initial radar results can be used to refine and/or disambiguate corresponding lidar results. Additionally, the initial results from one source can be used for cross-modal refinement to improve the subsequent detection results of the other source, such as by adjusting power usage, thresholds, and scan areas. For example, the power used for lidar can be increased or decreased depending on radar measurements, and the thresholds used to detect valid measurements can be similarly adjusted. Additional passes over a refined area or region can be performed much earlier than with decoupled systems, such as where fusion of lidar and radar data is performed after a lidar point cloud is generated. In contrast, the refinement process using the disclosed inventions can be performed earlier and iteratively such as on selective and identified dedicated regions of interest over a configurable number of passes. This cross-modal approach applies to all supported modalities, including scenarios where lidar excels over radar. When one modality excels for a particular region of interest, the region can be rescanned with adjusted configuration parameters such as increased power and modified threshold values based on sensor measurements from the modality that is initially found to be more accurate.
In various embodiments, the improved accuracy of the disclosed integrated lidar and radar system allows the lidar and radar functionality to each operate with a higher tolerance to noise. For example, when operated in fog, radar can continue to penetrate through the fog even when lidar can be impacted by the fog due to increased noise such as back scatter from fog. When integrated using the disclosed integrated lidar and radar system, the integrated radar can provide an initial view of the surrounding environment and function as a source of validation for results from the integrated lidar. The results from the integrated lidar, once validated with radar readings, can provide a more accurate scan of the environment than can be made with radar alone.
In some embodiments, the disclosed integrated lidar and radar system includes a dual mode scanner that can function to perform scanning for both lidar and radar purposes. For example, a dual mode scanner can include one or more shared scanning mirrors that allow the light pulses and RF signals to be coupled along one or more axes. In some embodiments, the emitted light pulses and RF signals can be reflected off the same or different facets of a polygon mirror of the dual mode scanner to direct the corresponding emitted light pulses and RF signals at synchronized azimuth angles. Similarly, the emitted light pulses and RF signals can be reflected off the same scanning mirror to direct the corresponding emitted light pulses and RF signals at synchronized elevation angles. In some embodiments, although the lidar and radar measurements are synchronized, they may be decoupled along one or more axes. For example, a scanning mirror can couple the light pulses and RF signals at synchronized azimuth angles and a corresponding elevation scanning mirror that is reflective for light but transmissive to RF signals can decouple the light pulses from the RF signal to direct each at different elevation angles. In particular embodiments, the mechanical steering performed by the dual mode scanner is combined with electronic steering. For example, by combining mechanical and electronic scanning techniques, the lidar and radar elements can be coupled along some axes and controlled independently along other decoupled axes. In some embodiments, light pulses and RF signals are coupled at synchronized azimuth angles but decoupled in elevation. For example, the light pulses can be scanned in elevation using a scanning mirror transmissive to RF signals and the RF signals can be electronically scanned in elevation.
In various embodiments, different scanning configurations of the dual mode scanner are appropriate and the different configurations allow different results to be achieved. Although the light pulses and RF signals may be coupled or decoupled for different axes, the corresponding light and RF sources can be synchronized with respect to timing. For example, the emitted light pulses and corresponding transmitted RF signals can be configured to exit the disclosed integrated lidar and radar system within a small transmission window, such as within nanoseconds of one another. The ability to synchronize the lidar and radar functionality, in both time and space, allows the resulting detection and ranging measurements to be analyzed together. The processing can be performed early in the perception processing pipeline allowing for improved accuracy with reduced computational resource, hardware, and power requirements. The results of the disclosed integrated lidar and radar system are highly accurate fused measurements and the ability to generate a corresponding precise and unified point cloud, including 3D and/or 4D point clouds, from the fused measurements.
In some embodiments, an integrated lidar and radar system comprises a light source, a radar transmitter, a light receiver, a radar receiver, and a processor. For example, the integrated lidar and radar system performs both lidar and radar functionality with one or more dual mode elements, such as a processor and/or a dual mode scanner, that function for both lidar and radar purposes. In some embodiments, the light source is configured to emit a light pulse. For example, a light source can emit light pulses having one or more particular operating wavelengths. In some embodiments, the radar transmitter is configured to transmit a radar signal, wherein an emission direction of the light pulse of the light source and a transmission direction of the radar signal of the radar transmitter are at least in part synchronized. For example, a transmitted radar signal and an emitted light pulse can be coupled along one or more axes, such as directing the radar signal and light pulse to be synchronized along the same azimuth and/or elevation. In some embodiments, the lidar and radar are synchronized partially (along one axis) or more completely (along multiple axes) using a dual mode scanner. The dual mode scanner can include one or more mirrors including mirrors that reflect both light beams and RF signals as well as mirrors that reflect one but are transmissive to another, such as reflective for light pulses but transmissive for radar signals. In various embodiments, the synchronization of the transmitted radar signal and the emitted light includes synchronizing the timing of their transmission and/or reception. For example, the transmission of the radar signal and light pulse can be performed within nanoseconds of one another.
In some embodiments, the light receiver of the integrated lidar and radar system is configured to detect a reflected light pulse and the radar receiver of the integrated lidar and radar system is configured to detect a reflected radar signal. For example, a light receiver of the integrated lidar and radar system detects reflected light pulses from downrange objects and the radar receiver of the integrated lidar and radar system detects reflected radar signals of the same or different downrange objects. In some embodiments, the processor is configured to determine a dimensional representation of an environment based at least in part on the detected reflected light pulse and the detected reflected radar signal. For example, measurements outputted by corresponding light and RF detectors for the received reflections can be processed using the same processor to create a dimensional representation of the surrounding environment. In some embodiments, the dimensional representation corresponds to a point cloud and/or feature map of the surrounding environment.
In various embodiments, in the event the radar and lidar transmissions are at least partially synchronized, the measured values corresponding to the received associated reflections can be fused and, in some embodiments, fused early in a perception processing pipeline. For example, received radar and lidar detection data relating to the same downrange objects can be correlated to create highly accurate and precise object measurements. Moreover, the corresponding lidar and radar measurements of the integrated lidar and radar system can be fused early to generate a highly detailed point cloud particularly for specific regions of interest. Where the lidar and radar measurements do not overlap, such as when their respective transmissions are directed at different fields of regard, the measurements for different radar and lidar fields of regards can be used to generate a larger and more accurate point cloud. For example, the total scanned environment can be expanded and/or specific regions of interest, such as high impact and/or high value regions, can be generated with higher density lidar measurements and lower value regions, such as regions on the periphery, can be generated with lower density radar measurements.
In particular embodiments, by overlapping scanned fields of regards, the measured reflections of synchronized lidar and radar transmissions via integrated lidar and radar components improve the overall accuracy of the detection and ranging system. For example, a corresponding point cloud can be generated with a higher point density by at least in part validating the accuracy of target data using the multiple measurements captured from different sensors. In some embodiments, the ability to fuse radar and lidar measurements allows both radar and lidar components to be operated with higher thresholds for noise. Data that would otherwise be discarded, for example, as potential noise, can be confirmed as valid and accurate measurement data. These advantages are possible through the early fusion of coupled lidar and radar measurements using the disclosed integrated lidar and radar system.
An integrated lidar and radar system operates in a vehicle and includes multiple “eyes,” each of which has its own field of regard, or an angular range over which the eye scans targets using pulses of light and/or radio frequency (RF) signals in accordance with a scan pattern. The fields of regard can combine along a certain dimension (e.g., horizontally) to define the overall field of regard of the integrated lidar and radar system. The integrated lidar and radar system then can use data received via its eyes to generate a point cloud or otherwise process the received data.
In a two-eye configuration of the integrated lidar and radar system, the two eyes can be housed together and scan the respective fields of regard via a shared window or separate windows, or the eyes can be housed separately. In the latter case, an assembly referred to as a “sensor head” can include a scanner (including a dual mode scanner), a laser receiver, and an optical element such as a collimator or a laser diode to generate or convey a beam of light. The assembly further includes radar components to scan radio frequency (RF) signals using the dual mode scanner and a RF receiver and other elements to emit and receive portions of the emitted RF signals.
Depending on the implementation, each eye of an integrated lidar and radar system can include a separate scanner (e.g., each eye can be equipped with a pivotable scan mirror to scan the field of regard vertically and another pivotable scan mirror to scan the field of regard horizontally), a partially shared scanner (e.g., each eye can be equipped with a pivotable scan mirror to scan the field of regard vertically, and a shared polygon mirror can scan the corresponding fields of regard horizontally, using different reflective surfaces), or a fully shared scanner (e.g., a pivotable planar mirror can scan the fields of regard vertically by reflecting incident beams at different regions on the reflective surface, and a shared polygon mirror can scan the corresponding fields of regard horizontally, using different reflective surfaces). Each scanner can function in a dual mode to additionally scan radio frequency (RF) signals (in addition to light pulses or beams of light) as part of a radar system of an integrated lidar and radar system.
Different hardware configurations allow the integrated lidar and radar system to operate the eyes more independently of each other, as is the case with separate scanners, or less independently, as is the case with a fully shared scanner. For example, the two or more eyes may scan the respective fields of regard using similar or different scan patterns. In one implementation, the two eyes trace out the same pattern, but with a certain time differential to maintain angular separation between light-source fields of view and thereby reduce the probability of cross-talk events between the sensor heads. In another implementation, the two eyes scan the corresponding fields of regard according to different scan patterns, at least in some operational states (e.g., when the vehicle is turning right or left). In various embodiments, the scanners, whether separate, fully shared, and/or partially shared, can be dual mode scanners that scan both light pulses and radio frequency (RF) signals using one or more shared elements of the same dual mode scanner. The scan patterns for the light pulses and RF signals scanned via the same dual mode scanner can be similar or different scan patterns.
Further, according to one approach, two eyes of an integrated lidar and radar system are arranged so that the fields of regard of the eyes are adjacent and non-overlapping. For example, each field of regard can span approximately 60 degrees horizontally and 30 degrees vertically, so that the combined field of regard of the integrated lidar and radar system spans approximately 120 degrees horizontally and 30 degrees vertically. The corresponding scanners (or paths within a shared scanner) can point away from each other at a certain angle, for example, so that the respective fields of regard abut approximately at an axis corresponding to the forward-facing direction of the vehicle.
Alternatively, the integrated lidar and radar system can operate in a “cross-eyed” configuration to create an area of overlap between the fields of regard. The area of overlap can be approximately centered along the forward-facing direction or another direction, which in some implementations a controller can determine dynamically. In this implementation, the two sensor heads can yield a higher density of scan in the area that generally is more important. In some implementations, the fields of regard in a cross-eyed two-eye configuration are offset from each other by a half-pixel value, so that the area of overlap has twice as many pixels. In general, the fields of regard can overlap angularly or translationally. To reduce the probability of cross-talk events (e.g., the situation when a pulse emitted by the light source associated with the first eye is received by the receiver of the second eye), the integrated lidar and radar system can use output beams with different wavelengths.
As shown in
In some embodiments, light source 110 and radio frequency (RF) source 210 are sources for light pulses and RF signals, respectively, used to determine measurements of downrange objects such as target 130. For example, using light pulses emitted by light source 110 and RF signals transmitted by RF source 210, the distance D from integrated lidar and radar system 100 to target 130 can be determined. In some embodiments, RF source 210 corresponds to an array, a phased array, or another appropriate RF source. For example, in some embodiments, RF source 210 corresponds to a phased array RF source that can be electronically steered along with the configured mechanical steering performed by dual mode scanner 120.
In some embodiments, dual mode scanner 120 is a scanner that functions to scan both light pulses and radio frequency (RF) signals across one or more fields of regard. For example, dual mode scanner 120 controls the scanned fields of regard with respect to both lidar and radar with elements that allow the light and RF sources to be partially or fully coupled. In some embodiments, scanning performed by dual mode scanner 120 utilizes one or more scanning mirrors including one or more polygon and/or LATM mirrors for directing the azimuth and elevation angles of output light beam 125 and output radio frequency (RF) signal 225. In particular embodiments, the included scanning mirrors may be configured to couple light pulses and RF signals by reflecting both light and RF frequency signals or to decouple light pulses and RF signals by reflecting light and transmitting RF frequency signals. In some embodiments, the coating and/or materials of the mirror can be configured to focus and/or reflect light and RF signals differently. For example, a polygon with flat optical facets, but containing curved metallic surfaces within, can enable focusing and/or modifying the divergence of the radar beam. Based on the configuration of dual mode scanner 120, different and potentially overlapping lidar and radar fields of regard can be scanned when directing output light beam 125 and output radio frequency (RF) signal 225 from integrated lidar and radar system 100.
Once output light beam 125 and output radio frequency (RF) signal 225 reach the downrange target 130, the target 130 may scatter or reflect at least a portion of light from the output light beam 125 and at least a portion of the RF signal from output RF signal 225, and some of the scattered or reflected light and/or RF signal may return toward the integrated lidar and radar system 100. In the example of
In some embodiments, light receiver 140 is configured to receive or detect photons from input light beam 135 and produce one or more representative lidar signals. For example, the light receiver 140 may produce an output electrical signal 145 that is representative of the input light beam 135, and the electrical signal 145 may be sent to controller 150. Similarly, radio frequency (RF) receiver 240 is configured to receive or detect RF signals from input radio frequency (RF) signal 235 and produce one or more representative radar signals. For example, the RF receiver 240 may produce an output electrical signal 145 that is representative of the input RF signal 235, and the electrical signal 145 may be sent to controller 150. In particular embodiments, light receiver 140, RF receiver 240, and/or controller 150 may include a processor, computing system (e.g., an ASIC or FPGA), or other suitable circuitry. A controller 150 may be configured to analyze one or more characteristics including lidar and radar values of the electrical signal 145 from the light receiver 140 and/or RF receiver 240 to determine one or more characteristics of the target 130, such as its distance downrange from the integrated lidar and radar system 100. This may be done, for example, by analyzing a time of flight or a frequency or phase of a transmitted output light beam 125, a transmitted output radio frequency (RF) signal 225, a received input light beam 135, and/or a received input RF signal 235. If integrated lidar and radar system 100 measures a time of flight of T (e.g., T represents a round-trip time of flight for an emitted pulse of light or RF signal to travel from the integrated lidar and radar system 100 to the target 130 and back to the integrated lidar and radar system 100), then the distance D from the target 130 to the integrated lidar and radar system 100 may be expressed as D=c·T/2, where c is the speed of light (approximately 3.0×108 m/s). In particular embodiments, a distance D from integrated lidar and radar system 100 to a target 130 may be referred to as a distance, depth, or range of target 130. In some embodiments, light receiver 140 and/or RF receiver 240 utilize signals from the other respective component in determining measurements. For example, in various embodiments, light receiver 140 can utilize electrical signal 145 from RF receiver 240 and/or RF receiver 240 can utilize electrical signal 145 from light receiver 140.
In various embodiments, controller 150 fuses measurements provided by light receiver 140 and radio frequency (RF) receiver 240 to create a unified result. For example, measurements corresponding to the same target 130 can be correlated and fused by controller 150. In some embodiments, the provided measurements are used to determine which among a series of detected reflections to associate with a source light pulse or RF signal. For example, range warp issues can be resolved using together the measurements provided by light receiver 140 and RF receiver 240. In various embodiments, the measurements provided by light receiver 140 and RF receiver 240 to controller 150 correspond to electrical signal 145. The process of associating and fusing measurements from light receiver 140 and RF receiver 240 can correspond to a fusion step performed early in a perception pipeline for creating a dimensional representation of the surrounding and/or scanned environment. For example, early fused measurements determined by controller 150 can be used to construct a highly detailed point cloud and/or feature map of the surrounding environment.
In some embodiments, integrated lidar and radar system 100 may include a telescope, one or more lenses, one or more mirrors, and/or other lidar and/or radar elements (not shown). These additional components can be used, for example, to configure integrated lidar and radar system 100 to direct, expand, focus, collimate, or otherwise manipulate output light beam 125, output radio frequency (RF) signal 225, input light beam 135, and/or input radio frequency (RF) signal 235 as desired. As an example, the integrated lidar and radar system 100 may include one or more lenses to focus the input light beam 135 onto a photodetector of light receiver 140. As another example, the integrated lidar and radar system 100 may include one or more flat mirrors or curved mirrors (e.g., concave, convex, or parabolic mirrors) to steer or focus the output light beam 125, output RF signal 225, the input light beam 135, and/or input RF signal 235.
In various embodiments, the light source 110 may include, for example, a laser which emits light having a particular operating wavelength in the infrared, visible, or ultraviolet portions of the electromagnetic spectrum. As an example, light source 110 may include a laser with one or more operating wavelengths between approximately 900 nanometers (nm) and 2100 nm. The light source 110 emits an output light beam 125 which may be continuous wave (CW), pulsed, or modulated in any suitable manner for a given application. The output light beam 125 is directed downrange toward a remote target 130. As an example, the remote target 130 may be located a distance D of approximately 1 m to 1 km from the integrated lidar and radar system 100.
Once the output light beam 125 reaches the downrange target 130, the target may scatter or reflect at least a portion of light from the output light beam 125, and some of the scattered or reflected light may return toward the integrated lidar and radar system 100. In the example of
In particular embodiments, output light beam 125 may include or may be referred to as an optical signal, output optical signal, emitted optical signal, output light, emitted pulse of light, laser beam, light beam, optical beam, emitted beam, emitted light, or beam. In particular embodiments, input light beam 135 may include or may be referred to as a received optical signal, received pulse of light, input pulse of light, input optical signal, return beam, received beam, return light, received light, input light, scattered light, or reflected light. As used herein, scattered light may refer to light that is scattered or reflected by a target 130. As an example, an input light beam 135 may include: light from the output light beam 125 that is scattered by target 130; light from the output light beam 125 that is reflected by target 130; or a combination of scattered and reflected light from target 130.
In particular embodiments, light receiver 140 may receive or detect photons from input light beam 135 and produce one or more representative signals. For example, the light receiver 140 may produce an output electrical signal 145 that is representative of the input light beam 135, and the electrical signal 145 may be sent to controller 150. In particular embodiments, light receiver 140 or controller 150 may include a processor, computing system (e.g., an ASIC or FPGA), or other suitable circuitry. A controller 150 may be configured to analyze one or more characteristics of the electrical signal 145 from the light receiver 140 to determine one or more characteristics of the target 130, such as its distance downrange from the integrated lidar and radar system 100. This may be done, for example, by analyzing a time of flight or a frequency or phase of a transmitted beam of light 125 or a received input light beam 135. If integrated lidar and radar system 100 measures a time of flight of T (e.g., T represents a round-trip time of flight for an emitted pulse of light to travel from the integrated lidar and radar system 100 to the target 130 and back to the integrated lidar and radar system 100), then the distance D from the target 130 to the integrated lidar and radar system 100 may be expressed as D=c·T/2, where c is the speed of light (approximately 3.0×108 m/s). As an example, if a time of flight is measured to be T=300 ns, then the distance from the target 130 to the integrated lidar and radar system 100 may be determined to be approximately D=45.0 m. As another example, if a time of flight is measured to be T=1.33 μs, then the distance from the target 130 to the integrated lidar and radar system 100 may be determined to be approximately D=199.5 m. In particular embodiments, a distance D from integrated lidar and radar system 100 to a target 130 may be referred to as a distance, depth, or range of target 130. As used herein, the speed of light c refers to the speed of light in any suitable medium, such as for example in air, water, or vacuum. As an example, the speed of light in vacuum is approximately 2.9979×108 m/s, and the speed of light in air (which has a refractive index of approximately 1.0003) is approximately 2.9970×108 m/s.
In particular embodiments, light source 110 may include a pulsed or CW laser. As an example, light source 110 may be a pulsed laser configured to produce or emit pulses of light with a pulse duration or pulse width of approximately 10 picoseconds (ps) to 100 nanoseconds (ns). The pulses may have a pulse duration of approximately 100 ps, 200 ps, 400 ps, 1 ns, 2 ns, 5 ns, 10 ns, 20 ns, 50 ns, 100 ns, or any other suitable pulse duration. As another example, light source 110 may be a pulsed laser that produces pulses with a pulse duration of approximately 1-5 ns. As another example, light source 110 may be a pulsed laser that produces pulses at a pulse repetition frequency of approximately 80 kHz to 10 MHz or a pulse period (e.g., a time between consecutive pulses) of approximately 100 ns to 12.5 μs. In particular embodiments, light source 110 may have a substantially constant pulse repetition frequency, or light source 110 may have a variable or adjustable pulse repetition frequency. As an example, light source 110 may be a pulsed laser that produces pulses at a substantially constant pulse repetition frequency of approximately 640 kHz (e.g., 640,000 pulses per second), corresponding to a pulse period of approximately 1.56 μs. As another example, light source 110 may have a pulse repetition frequency (which may be referred to as a repetition rate) that can be varied from approximately 200 kHz to 3 MHz. As used herein, a pulse of light may be referred to as an optical pulse, a light pulse, or a pulse.
In particular embodiments, light source 110 may include a pulsed or CW laser that produces a free-space output light beam 125 having any suitable average optical power. As an example, output light beam 125 may have an average power of approximately 1 milliwatt (mW), 10 mW, 100 mW, 1 watt (W), 10 W, or any other suitable average power. In particular embodiments, output light beam 125 may include optical pulses with any suitable pulse energy or peak optical power. As an example, output light beam 125 may include pulses with a pulse energy of approximately 0.01 μJ, 0.1 μJ, 0.5 μJ, 1 μJ, 2 μJ, 10 μJ, 100 μJ, 1 mJ, or any other suitable pulse energy. As another example, output light beam 125 may include pulses with a peak power of approximately 10 W, 100 W, 1 kW, 5 kW, 10 kW, or any other suitable peak power. The peak power (Ppeak) of a pulse of light can be related to the pulse energy (E) by the expression E=Ppeak·Δt, where Δt is the duration of the pulse, and the duration of a pulse may be defined as the full width at half maximum duration of the pulse. For example, an optical pulse with a duration of 1 ns and a pulse energy of 1 μJ has a peak power of approximately 1 kW. The average power (Pav) of an output light beam 125 can be related to the pulse repetition frequency (PRF) and pulse energy by the expression Pav=PRF·E. For example, if the pulse repetition frequency is 500 kHz, then the average power of an output light beam 125 with 1-μJ pulses is approximately 0.5 W.
In particular embodiments, light source 110 may include a laser diode, such as for example, a Fabry-Perot laser diode, a quantum well laser, a distributed Bragg reflector (DBR) laser, a distributed feedback (DFB) laser, a vertical-cavity surface-emitting laser (VCSEL), a quantum dot laser diode, a grating-coupled surface-emitting laser (GCSEL), a slab-coupled optical waveguide laser (SCOWL), a single-transverse-mode laser diode, a multi-mode broad area laser diode, a laser-diode bar, a laser-diode stack, or a tapered-stripe laser diode. As an example, light source 110 may include an aluminum-gallium-arsenide (AlGaAs) laser diode, an indium-gallium-arsenide (InGaAs) laser diode, an indium-gallium-arsenide-phosphide (InGaAsP) laser diode, or a laser diode that includes any suitable combination of aluminum (Al), indium (In), gallium (Ga), arsenic (As), phosphorous (P), or any other suitable material. In particular embodiments, light source 110 may include a pulsed or CW laser diode with a peak emission wavelength between 1200 nm and 1600 nm. As an example, light source 110 may include a current-modulated InGaAsP DFB laser diode that produces optical pulses at a wavelength of approximately 1550 nm. As another example, light source 110 may include a laser diode that emits light at a wavelength between 1500 nm and 1510 nm.
In particular embodiments, light source 110 may include a pulsed or CW laser diode followed by one or more optical-amplification stages. For example, a seed laser diode may produce a seed optical signal, and an optical amplifier may amplify the seed optical signal to produce an amplified optical signal that is emitted by the light source 110. In particular embodiments, an optical amplifier may include a fiber-optic amplifier or a semiconductor optical amplifier (SOA). For example, a pulsed laser diode may produce relatively low-power optical seed pulses which are amplified by a fiber-optic amplifier. As another example, a light source 110 may include a fiber-laser module that includes a current-modulated laser diode with an operating wavelength of approximately 1550 nm followed by a single-stage or a multi-stage erbium-doped fiber amplifier (EDFA) or erbium-ytterbium-doped fiber amplifier (EYDFA) that amplifies the seed pulses from the laser diode. As another example, light source 110 may include a continuous-wave (CW) or quasi-CW laser diode followed by an external optical modulator (e.g., an electro-optic amplitude modulator). The optical modulator may modulate the CW light from the laser diode to produce optical pulses which are sent to a fiber-optic amplifier or SOA. As another example, light source 110 may include a pulsed or CW seed laser diode followed by a semiconductor optical amplifier (SOA). The SOA may include an active optical waveguide configured to receive a seed optical signal (e.g., pulses of light or CW light) from the seed laser diode and amplify the seed optical signal as it propagates through the waveguide. For example, the seed laser diode may produce relatively low-power seed optical pulses, and the SOA may amplify each seed optical pulse to produce an emitted pulse of light. The optical gain of the SOA may be provided by pulsed or direct-current (DC) electrical current supplied to the SOA. The SOA may be integrated on the same chip as the seed laser diode, or the SOA may be a separate device with an anti-reflection coating on its input facet or output facet. As another example, light source 110 may include a seed laser diode followed by an SOA, which in turn is followed by a fiber-optic amplifier. For example, the seed laser diode may produce relatively low-power seed optical pulses which are amplified by the SOA, and the fiber-optic amplifier may further amplify each of the optical pulses to produce emitted pulses of light.
In particular embodiments, light source 110 may include a direct-emitter laser diode. A direct-emitter laser diode (which may be referred to as a direct emitter) may include a laser diode which produces light that is not subsequently amplified by an optical amplifier. A light source 110 that includes a direct-emitter laser diode may not include an optical amplifier, and the output light produced by a direct emitter may not be amplified after it is emitted by the laser diode. The light produced by a direct-emitter laser diode (e.g., optical pulses, CW light, or frequency-modulated light) may be emitted directly as a free-space output light beam 125 without being amplified. A direct-emitter laser diode may be driven by an electrical power source that supplies current pulses to the laser diode, and each current pulse may result in the emission of an output optical pulse.
In particular embodiments, light source 110 may include a diode-pumped solid-state (DPSS) laser. A DPSS laser (which may be referred to as a solid-state laser) may refer to a laser that includes a solid-state, glass, ceramic, or crystal-based gain medium that is pumped by one or more pump laser diodes. The gain medium may include a host material that is doped with rare-earth ions (e.g., neodymium, erbium, ytterbium, or praseodymium). For example, a gain medium may include a yttrium aluminum garnet (YAG) crystal that is doped with neodymium (Nd) ions, and the gain medium may be referred to as a Nd:YAG crystal. A DPSS laser with a Nd:YAG gain medium may produce light at a wavelength between approximately 1300 nm and approximately 1400 nm, and the Nd:YAG gain medium may be pumped by one or more pump laser diodes with an operating wavelength between approximately 730 nm and approximately 900 nm. A DPSS laser may be a passively Q-switched laser that includes a saturable absorber (e.g., a vanadium-doped crystal that acts as a saturable absorber). Alternatively, a DPSS laser may be an actively Q-switched laser that includes an active Q-switch (e.g., an acousto-optic modulator or an electro-optic modulator). A passively or actively Q-switched DPSS laser may produce output optical pulses that form an output light beam 125 of an integrated lidar and radar system 100.
In particular embodiments, an output beam of light 125 emitted by light source 110 may be a collimated optical beam having any suitable beam divergence, such as for example, a full-angle beam divergence of approximately 0.5 to 10 milliradians (mrad). A divergence of output light beam 125 may refer to an angular measure of an increase in beam size (e.g., a beam radius or beam diameter) as output light beam 125 travels away from light source 110 or integrated lidar and radar system 100. In particular embodiments, output light beam 125 may have a substantially circular cross section with a beam divergence characterized by a single divergence value. As an example, an output light beam 125 with a circular cross section and a full-angle beam divergence of 2 mrad may have a beam diameter or spot size of approximately 20 cm at a distance of 100 m from integrated lidar and radar system 100. In particular embodiments, output light beam 125 may have a substantially elliptical cross section characterized by two divergence values. As an example, output light beam 125 may have a fast axis and a slow axis, where the fast-axis divergence is greater than the slow-axis divergence. As another example, output light beam 125 may be an elliptical beam with a fast-axis divergence of 4 mrad and a slow-axis divergence of 2 mrad.
In particular embodiments, an output light beam 125 emitted by light source 110 may be unpolarized or randomly polarized, may have no specific or fixed polarization (e.g., the polarization may vary with time), or may have a particular polarization (e.g., output light beam 125 may be linearly polarized, elliptically polarized, or circularly polarized). As an example, light source 110 may produce light with no specific polarization or may produce light that is linearly polarized.
In particular embodiments, integrated lidar and radar system 100 may include one or more optical components configured to reflect, focus, filter, shape, modify, steer, or direct light within the integrated lidar and radar system 100 or light produced or received by the integrated lidar and radar system 100 (e.g., output light beam 125 or input light beam 135). As an example, integrated lidar and radar system 100 may include one or more lenses, mirrors, filters (e.g., bandpass or interference filters), beam splitters, optical splitters, polarizers, polarizing beam splitters, wave plates (e.g., half-wave or quarter-wave plates), diffractive elements, holographic elements, isolators, couplers, detectors, beam combiners, or collimators. The optical components in an integrated lidar and radar system 100 may be free-space optical components, fiber-coupled optical components, or a combination of free-space and fiber-coupled optical components.
In particular embodiments, integrated lidar and radar system 100 may include a telescope, one or more lenses, or one or more mirrors configured to expand, focus, or collimate the output light beam 125 or the input light beam 135 to a desired beam diameter or divergence. As an example, the integrated lidar and radar system 100 may include one or more lenses to focus the input light beam 135 onto a photodetector of light receiver 140. As another example, the integrated lidar and radar system 100 may include one or more flat mirrors or curved mirrors (e.g., concave, convex, or parabolic mirrors) to steer or focus the output light beam 125 or the input light beam 135. For example, the integrated lidar and radar system 100 may include an off-axis parabolic mirror to focus the input light beam 135 onto a photodetector of light receiver 140. As illustrated in
In particular embodiments, mirror 115 may provide for output light beam 125 and input light beam 135 to be substantially coaxial so that the two beams travel along approximately the same optical path (albeit in opposite directions). The input and output beams being substantially coaxial may refer to the beams being at least partially overlapped or sharing a common propagation axis so that input light beam 135 and output light beam 125 travel along substantially the same optical path (albeit in opposite directions). As an example, output light beam 125 and input light beam 135 may be parallel to each other to within less than 10 mrad, 5 mrad, 2 mrad, 1 mrad, 0.5 mrad, or 0.1 mrad. As output light beam 125 is scanned across a field of regard, the input light beam 135 may follow along with the output light beam 125 so that the coaxial relationship between the two beams is maintained.
In particular embodiments, integrated lidar and radar system 100 may include a dual mode scanner 120 configured to scan an output light beam 125 across a field of regard of the integrated lidar and radar system 100. As an example, dual mode scanner 120 may include one or more scanning mirrors configured to pivot, rotate, oscillate, or move in an angular manner about one or more rotation axes. The output light beam 125 may be reflected by a scanning mirror, and as the scanning mirror pivots or rotates, the reflected output light beam 125 may be scanned in a corresponding angular manner. As an example, a scanning mirror may be configured to periodically pivot back and forth over a 30-degree range, which results in the output light beam 125 scanning back and forth across a 60-degree range (e.g., a Θ-degree rotation by a scanning mirror results in a 2Θ-degree angular scan of output light beam 125).
In particular embodiments, a scanning mirror (which may be referred to as a scan mirror) may be attached to or mechanically driven by a scanner actuator or mechanism which pivots or rotates the mirror over a particular angular range (e.g., over a 5° angular range, 30° angular range, 60° angular range, 120° angular range, 360° angular range, or any other suitable angular range). A scanner actuator or mechanism configured to pivot or rotate a mirror may include a galvanometer scanner, a resonant scanner, a piezoelectric actuator, a voice coil motor, an electric motor (e.g., a DC motor, a brushless DC motor, a synchronous electric motor, or a stepper motor), a microelectromechanical systems (MEMS) device, or any other suitable actuator or mechanism. As an example, a dual mode scanner 120 may include a scanning mirror attached to a galvanometer scanner configured to pivot back and forth over a 1° to 30° angular range. As another example, a dual mode scanner 120 may include a scanning mirror that is attached to or is part of a MEMS device configured to scan over a 1° to 30° angular range. As another example, a dual mode scanner 120 may include a polygon mirror configured to rotate continuously in the same direction (e.g., rather than pivoting back and forth, the polygon mirror continuously rotates 360 degrees in a clockwise or counterclockwise direction). The polygon mirror may be coupled or attached to a synchronous motor configured to rotate the polygon mirror at a substantially fixed rotational frequency (e.g., a rotational frequency of approximately 1 Hz, 10 Hz, 50 Hz, 100 Hz, 500 Hz, or 1,000 Hz).
In particular embodiments, dual mode scanner 120 may be configured to scan the output light beam 125 (which may include at least a portion of the light emitted by light source 110) across a field of regard of the integrated lidar and radar system 100. A field of regard (FOR) of an integrated lidar and radar system 100 may refer to an area, region, or angular range over which the integrated lidar and radar system 100 may be configured to scan or capture distance information. As an example, an integrated lidar and radar system 100 with an output light beam 125 with a 30-degree scanning range may be referred to as having a 30-degree angular field of regard. As another example, an integrated lidar and radar system 100 with a scanning mirror that rotates over a 30-degree range may produce an output light beam 125 that scans across a 60-degree range (e.g., a 60-degree fOR). In particular embodiments, integrated lidar and radar system 100 may have a FOR of approximately 10°, 20°, 40°, 60°, 120°, 360°, or any other suitable FOR.
In particular embodiments, dual mode scanner 120 may be configured to scan the output light beam 125 horizontally and vertically, and integrated lidar and radar system 100 may have a particular FOR along the horizontal direction and another particular FOR along the vertical direction. As an example, integrated lidar and radar system 100 may have a horizontal FOR of 10° to 120° and a vertical FOR of 2° to 45°. In particular embodiments, dual mode scanner 120 may include a first scan mirror and a second scan mirror, where the first scan mirror directs the output light beam 125 toward the second scan mirror, and the second scan mirror directs the output light beam 125 downrange from the integrated lidar and radar system 100. As an example, the first scan mirror may scan the output light beam 125 along a first direction, and the second scan mirror may scan the output light beam 125 along a second direction that is different from the first direction (e.g., the second direction may be substantially orthogonal to the first direction). As another example, the first scan mirror may scan the output light beam 125 along a substantially horizontal direction, and the second scan mirror may scan the output light beam 125 along a substantially vertical direction (or vice versa). As another example, the first and second scan mirrors may each be driven by galvanometer scanners. As another example, the first or second scan mirror may include a polygon mirror driven by an electric motor. In particular embodiments, dual mode scanner 120 may be referred to as a beam scanner, optical scanner, or laser scanner.
In particular embodiments, one or more scanning mirrors may be communicatively coupled to controller 150 which may control the scanning mirror(s) so as to guide the output light beam 125 in a desired direction downrange or along a desired scan pattern. In particular embodiments, a scan pattern may refer to a pattern or path along which the output light beam 125 is directed. As an example, dual mode scanner 120 may include two scanning mirrors configured to scan the output light beam 125 across a 60° horizontal FOR and a 20° vertical FOR. The two scanner mirrors may be controlled to follow a scan path that substantially covers the 60°×20° FOR. As an example, the scan path may result in a point cloud with pixels that substantially cover the 60°×20° FOR. The pixels may be approximately evenly distributed across the 60°×20° FOR. Alternatively, the pixels may have a particular nonuniform distribution (e.g., the pixels may be distributed across all or a portion of the 60°×20° FOR, and the pixels may have a higher density in one or more particular regions of the 60°×20° FOR).
In particular embodiments, an integrated lidar and radar system 100 may include a dual mode scanner 120 with a solid-state scanning device. A solid-state scanning device may refer to a dual mode scanner 120 that scans an output light beam 125 without the use of moving parts (e.g., without the use of a mechanical scanner, such as a mirror that rotates or pivots). For example, a solid-state dual mode scanner 120 may include one or more of the following: an optical phased array scanning device; a liquid-crystal scanning device; or a liquid lens scanning device. A solid-state dual mode scanner 120 may be an electrically addressable device that scans an output light beam 125 along one axis (e.g., horizontally) or along two axes (e.g., horizontally and vertically). In particular embodiments, a dual mode scanner 120 may include a solid-state scanner and a mechanical scanner. For example, a dual mode scanner 120 may include an optical phased array scanner configured to scan an output light beam 125 in one direction and a galvanometer scanner that scans the output light beam 125 in an orthogonal direction. The optical phased array scanner may scan the output beam relatively rapidly in a horizontal direction across the field of regard (e.g., at a scan rate of 50 to 1,000 scan lines per second), and the galvanometer may pivot a mirror at a rate of 1-30 Hz to scan the output light beam 125 vertically.
In particular embodiments, an integrated lidar and radar system 100 may include a light source 110 configured to emit pulses of light and a dual mode scanner 120 configured to scan at least a portion of the emitted pulses of light across a field of regard of the integrated lidar and radar system 100. One or more of the emitted pulses of light may be scattered by a target 130 located downrange from the integrated lidar and radar system 100, and a light receiver 140 may detect at least a portion of the pulses of light scattered by the target 130. A light receiver 140 may be referred to as a photoreceiver, optical receiver, optical sensor, detector, photodetector, or optical detector. In particular embodiments, integrated lidar and radar system 100 may include a light receiver 140 that receives or detects at least a portion of input light beam 135 and produces an electrical signal that corresponds to input light beam 135. As an example, if input light beam 135 includes an optical pulse, then light receiver 140 may produce an electrical current or voltage pulse that corresponds to the optical pulse detected by light receiver 140. As another example, light receiver 140 may include one or more avalanche photodiodes (APDs) or one or more single-photon avalanche diodes (SPADs). As another example, light receiver 140 may include one or more PN photodiodes (e.g., a photodiode structure formed by a p-type semiconductor and an n-type semiconductor, where the PN acronym refers to the structure having p-doped and n-doped regions) or one or more PIN photodiodes (e.g., a photodiode structure formed by an undoped intrinsic semiconductor region located between p-type and n-type regions, where the PIN acronym refers to the structure having p-doped, intrinsic, and n-doped regions). An APD, SPAD, PN photodiode, or PIN photodiode may each be referred to as a detector, photodetector, or photodiode. A detector may have an active region or an avalanche-multiplication region that includes silicon, germanium, InGaAs, InAsSb (indium arsenide antimonide), AlAsSb (aluminum arsenide antimonide), or AlInAsSb (aluminum indium arsenide antimonide). The active region may refer to an area over which a detector may receive or detect input light. An active region may have any suitable size or diameter, such as for example, a diameter of approximately 10 μm, 25 μm, 50 μm, 80 μm, 100 μm, 200 μm, 500 μm, 1 mm, 2 mm, or 5 mm.
In particular embodiments, light receiver 140 may include electronic circuitry that performs signal amplification, sampling, filtering, signal conditioning, analog-to-digital conversion, time-to-digital conversion, pulse detection, threshold detection, rising-edge detection, or falling-edge detection. As an example, light receiver 140 may include a transimpedance amplifier that converts a received photocurrent (e.g., a current produced by an APD in response to a received optical signal) into a voltage signal. The voltage signal may be sent to signal-detection circuitry that produces an analog or digital output signal 145 that corresponds to one or more optical characteristics (e.g., rising edge, falling edge, amplitude, duration, or energy) of a received optical pulse. As an example, the signal-detection circuitry may perform a time-to-digital conversion to produce a digital output signal 145. The electrical output signal 145 may be sent to controller 150 for processing or analysis (e.g., to determine a time-of-flight value corresponding to a received optical pulse).
In particular embodiments, a controller 150 (which may include or may be referred to as a processor, an FPGA, an ASIC, a computer, or a computing system) may be located within an integrated lidar and radar system 100 or outside of an integrated lidar and radar system 100. Alternatively, one or more parts of a controller 150 may be located within an integrated lidar and radar system 100, and one or more other parts of a controller 150 may be located outside an integrated lidar and radar system 100. In particular embodiments, one or more parts of a controller 150 may be located within a light receiver 140 of an integrated lidar and radar system 100, and one or more other parts of a controller 150 may be located in other parts of the integrated lidar and radar system 100. For example, a light receiver 140 may include an FPGA or ASIC configured to process an output electrical signal from the light receiver 140, and the processed signal may be sent to a computing system located elsewhere within the integrated lidar and radar system 100 or outside the integrated lidar and radar system 100. In particular embodiments, a controller 150 may include any suitable arrangement or combination of logic circuitry, analog circuitry, or digital circuitry.
In particular embodiments, controller 150 may be electrically coupled or communicatively coupled to light source 110, dual mode scanner 120, or light receiver 140. As an example, controller 150 may receive electrical trigger pulses or edges from light source 110, where each pulse or edge corresponds to the emission of an optical pulse by light source 110. As another example, controller 150 may provide instructions, a control signal, or a trigger signal to light source 110 indicating when light source 110 should produce optical pulses. Controller 150 may send an electrical trigger signal that includes electrical pulses, where each electrical pulse results in the emission of an optical pulse by light source 110. In particular embodiments, the frequency, period, duration, pulse energy, peak power, average power, or wavelength of the optical pulses produced by light source 110 may be adjusted based on instructions, a control signal, or trigger pulses provided by controller 150. In particular embodiments, controller 150 may be coupled to light source 110 and light receiver 140, and controller 150 may determine a time-of-flight value for an optical pulse based on timing information associated with when the pulse was emitted by light source 110 and when a portion of the pulse (e.g., input light beam 135) was detected or received by light receiver 140. In particular embodiments, controller 150 may include circuitry that performs signal amplification, sampling, filtering, signal conditioning, analog-to-digital conversion, time-to-digital conversion, pulse detection, threshold detection, rising-edge detection, or falling-edge detection.
In particular embodiments, integrated lidar and radar system 100 may include one or more processors (e.g., a controller 150) configured to determine a distance D from the integrated lidar and radar system 100 to a target 130 based at least in part on a round-trip time of flight for an emitted pulse of light to travel from the integrated lidar and radar system 100 to the target 130 and back to the integrated lidar and radar system 100. The target 130 may be at least partially contained within a field of regard of the integrated lidar and radar system 100 and located a distance D from the integrated lidar and radar system 100 that is less than or equal to an operating range (ROP) of the integrated lidar and radar system 100. In particular embodiments, an operating range (which may be referred to as an operating distance) of an integrated lidar and radar system 100 may refer to a distance over which the integrated lidar and radar system 100 is configured to sense or identify targets 130 located within a field of regard of the integrated lidar and radar system 100. The operating range of integrated lidar and radar system 100 may be any suitable distance, such as for example, 25 m, 50 m, 100 m, 200 m, 250 m, 500 m, or 1 km. As an example, an integrated lidar and radar system 100 with a 200-m operating range may be configured to sense or identify various targets 130 located up to 200 m away from the integrated lidar and radar system 100. The operating range ROP of an integrated lidar and radar system 100 may be related to the time T between the emission of successive optical signals by the expression ROP=c·τ/2. For an integrated lidar and radar system 100 with a 200-m operating range (ROP=200 m), the time T between successive pulses (which may be referred to as a pulse period, a pulse repetition interval (PRI), or a time period between pulses) is approximately 2 ROP/c≅1.33 μs. The pulse period T may also correspond to the time of flight for a pulse to travel to and from a target 130 located a distance ROP from the integrated lidar and radar system 100. Additionally, the pulse period T may be related to the pulse repetition frequency (PRY) by the expression τ=1/PRF. For example, a pulse period of 1.33 μs corresponds to a PRF of approximately 752 kHz.
In particular embodiments, an integrated lidar and radar system 100 may be used to determine the distance to one or more downrange targets 130. By scanning the integrated lidar and radar system 100 across a field of regard, the system may be used to map the distance to a number of points within the field of regard. Each of these depth-mapped points may be referred to as a pixel or a voxel. A collection of pixels captured in succession (which may be referred to as a depth map, a point cloud, or a frame) may be rendered as an image or may be analyzed to identify or detect objects or to determine a shape or distance of objects within the FOR. As an example, a point cloud may cover a field of regard that extends 600 horizontally and 150 vertically, and the point cloud may include a frame of 100-2000 pixels in the horizontal direction by 4-400 pixels in the vertical direction.
In particular embodiments, integrated lidar and radar system 100 may be configured to repeatedly capture or generate point clouds of a field of regard at any suitable frame rate between approximately 0.1 frames per second (FPS) and approximately 1,000 FPS. As an example, integrated lidar and radar system 100 may generate point clouds at a frame rate of approximately 0.1 FPS, 0.5 FPS, 1 FPS, 2 FPS, 5 FPS, 10 FPS, 20 FPS, 100 FPS, 500 FPS, or 1,000 FPS. As another example, integrated lidar and radar system 100 may be configured to produce optical pulses at a rate of 5×105 pulses/second (e.g., the system may determine 500,000 pixel distances per second) and scan a frame of 1000×50 pixels (e.g., 50,000 pixels/frame), which corresponds to a point-cloud frame rate of 10 frames per second (e.g., 10 point clouds per second). In particular embodiments, a point-cloud frame rate may be substantially fixed, or a point-cloud frame rate may be dynamically adjustable. As an example, an integrated lidar and radar system 100 may capture one or more point clouds at a particular frame rate (e.g., 1 Hz) and then switch to capture one or more point clouds at a different frame rate (e.g., 10 Hz). A slower frame rate (e.g., 1 Hz) may be used to capture one or more high-resolution point clouds, and a faster frame rate (e.g., 10 Hz) may be used to rapidly capture multiple lower-resolution point clouds.
In particular embodiments, an integrated lidar and radar system 100 may be configured to sense, identify, or determine distances to one or more targets 130 within a field of regard. As an example, an integrated lidar and radar system 100 may determine a distance to a target 130, where all or part of the target 130 is contained within a field of regard of the integrated lidar and radar system 100. All or part of a target 130 being contained within a FOR of the integrated lidar and radar system 100 may refer to the FOR overlapping, encompassing, or enclosing at least a portion of the target 130. In particular embodiments, target 130 may include all or part of an object that is moving or stationary relative to integrated lidar and radar system 100. As an example, target 130 may include all or a portion of a person, vehicle, motorcycle, truck, train, bicycle, wheelchair, pedestrian, animal, road sign, traffic light, lane marking, road-surface marking, parking space, pylon, guard rail, traffic barrier, pothole, railroad crossing, obstacle in or near a road, curb, stopped vehicle on or beside a road, utility pole, house, building, trash can, mailbox, tree, any other suitable object, or any suitable combination of all or part of two or more objects. In particular embodiments, a target may be referred to as an object.
In particular embodiments, light source 110, dual mode scanner 120, and light receiver 140 may be packaged together within a single housing, where a housing may refer to a box, case, or enclosure that holds or contains all or part of an integrated lidar and radar system 100. As an example, a lidar-system enclosure may contain a light source 110, mirror 115, dual mode scanner 120, and light receiver 140 of an integrated lidar and radar system 100. Additionally, the lidar-system enclosure may include a controller 150. The lidar-system enclosure may also include one or more electrical connections for conveying electrical power or electrical signals to or from the enclosure. In particular embodiments, one or more components of an integrated lidar and radar system 100 may be located remotely from a lidar-system enclosure. As an example, all or part of light source 110 may be located remotely from a lidar-system enclosure, and pulses of light produced by the light source 110 may be conveyed to the enclosure via optical fiber. As another example, all or part of a controller 150 may be located remotely from a lidar-system enclosure.
In particular embodiments, light source 110 may include an eye-safe laser, or integrated lidar and radar system 100 may be classified as an eye-safe laser system or laser product. An eye-safe laser, laser system, or laser product may refer to a system that includes a laser with an emission wavelength, average power, peak power, peak intensity, pulse energy, beam size, beam divergence, exposure time, or scanned output beam such that emitted light from the system presents little or no possibility of causing damage to a person's eyes. As an example, light source 110 or integrated lidar and radar system 100 may be classified as a Class 1 laser product (as specified by the 60825-1:2014 standard of the International Electrotechnical Commission (IEC)) or a Class I laser product (as specified by Title 21, Section 1040.10 of the United States Code of Federal Regulations (CFR)) that is safe under all conditions of normal use. In particular embodiments, integrated lidar and radar system 100 may be an eye-safe laser product (e.g., with a Class 1 or Class I classification) configured to operate at any suitable wavelength between approximately 900 nm and approximately 2100 nm. As an example, integrated lidar and radar system 100 may include a laser with an operating wavelength between approximately 1200 nm and approximately 1400 nm or between approximately 1400 nm and approximately 1600 nm, and the laser or the integrated lidar and radar system 100 may be operated in an eye-safe manner. As another example, integrated lidar and radar system 100 may be an eye-safe laser product that includes a scanned laser with an operating wavelength between approximately 900 nm and approximately 1700 nm. As another example, integrated lidar and radar system 100 may be a Class 1 or Class I laser product that includes a laser diode, fiber laser, or solid-state laser with an operating wavelength between approximately 1200 nm and approximately 1600 nm. As another example, integrated lidar and radar system 100 may have operating wavelengths between approximately 1500 nm and approximately 1550 nm.
In particular embodiments, one or more integrated lidar and radar systems 100 may be integrated into a vehicle. As an example, multiple integrated lidar and radar systems 100 may be integrated into a car to provide a complete 360-degree horizontal FOR around the car. As another example, 2-10 integrated lidar and radar systems 100, each system having a 45-degree to 180-degree horizontal FOR, may be combined together to form a sensing system that provides a point cloud covering a 360-degree horizontal FOR. The integrated lidar and radar systems 100 may be oriented so that adjacent FORs have an amount of spatial or angular overlap to allow data from the multiple integrated lidar and radar systems 100 to be combined or stitched together to form a single or continuous 360-degree point cloud. As an example, the FOR of each integrated lidar and radar system 100 may have approximately 1-30 degrees of overlap with an adjacent FOR. In particular embodiments, a vehicle may refer to a mobile machine configured to transport people or cargo. For example, a vehicle may include, may take the form of, or may be referred to as a car, automobile, motor vehicle, truck, bus, van, trailer, off-road vehicle, farm vehicle, lawn mower, construction equipment, forklift, robot, golf cart, motorhome, taxi, motorcycle, scooter, bicycle, skateboard, train, snowmobile, watercraft (e.g., a ship or boat), aircraft (e.g., a fixed-wing aircraft, helicopter, or dirigible), unmanned aerial vehicle (e.g., drone), or spacecraft. In particular embodiments, a vehicle may include an internal combustion engine or an electric motor that provides propulsion for the vehicle.
In particular embodiments, one or more integrated lidar and radar systems 100 may be included in a vehicle as part of an advanced driver assistance system (ADAS) to assist a driver of the vehicle in operating the vehicle. For example, an integrated lidar and radar system 100 may be part of an ADAS that provides information (e.g., about the surrounding environment) or feedback to a driver (e.g., to alert the driver to potential problems or hazards) or that automatically takes control of part of a vehicle (e.g., a braking system or a steering system) to avoid collisions or accidents. An integrated lidar and radar system 100 may be part of a vehicle ADAS that provides adaptive cruise control, automated braking, automated parking, collision avoidance, alerts the driver to hazards or other vehicles, maintains the vehicle in the correct lane, or provides a warning if an object or another vehicle is in a blind spot.
In particular embodiments, one or more integrated lidar and radar systems 100 may be integrated into a vehicle as part of an autonomous-vehicle driving system. As an example, an integrated lidar and radar system 100 may provide information about the surrounding environment to a driving system of an autonomous vehicle. An autonomous-vehicle driving system may be configured to guide the autonomous vehicle through an environment surrounding the vehicle and toward a destination. An autonomous-vehicle driving system may include one or more computing systems that receive information from an integrated lidar and radar system 100 about the surrounding environment, analyze the received information, and provide control signals to the vehicle's driving systems (e.g., steering mechanism, accelerator, brakes, lights, or turn signals). As an example, an integrated lidar and radar system 100 integrated into an autonomous vehicle may provide an autonomous-vehicle driving system with a point cloud every 0.1 seconds (e.g., the point cloud has a 10 Hz update rate, representing 10 frames per second). The autonomous-vehicle driving system may analyze the received point clouds to sense or identify targets 130 and their respective locations, distances, or speeds, and the autonomous-vehicle driving system may update control signals based on this information. As an example, if integrated lidar and radar system 100 detects a vehicle ahead that is slowing down or stopping, the autonomous-vehicle driving system may send instructions to release the accelerator and apply the brakes.
In particular embodiments, an autonomous vehicle may be referred to as an autonomous car, driverless car, self-driving car, robotic car, or unmanned vehicle. In particular embodiments, an autonomous vehicle may refer to a vehicle configured to sense its environment and navigate or drive with little or no human input. As an example, an autonomous vehicle may be configured to drive to any suitable location and control or perform all safety-critical functions (e.g., driving, steering, braking, parking) for the entire trip, with the driver not expected to control the vehicle at any time. As another example, an autonomous vehicle may allow a driver to safely turn their attention away from driving tasks in particular environments (e.g., on freeways), or an autonomous vehicle may provide control of a vehicle in all but a few environments, requiring little or no input or attention from the driver.
In particular embodiments, an autonomous vehicle may be configured to drive with a driver present in the vehicle, or an autonomous vehicle may be configured to operate the vehicle with no driver present. As an example, an autonomous vehicle may include a driver's seat with associated controls (e.g., steering wheel, accelerator pedal, and brake pedal), and the vehicle may be configured to drive with no one seated in the driver's seat or with little or no input from a person seated in the driver's seat. As another example, an autonomous vehicle may not include any driver's seat or associated driver's controls, and the vehicle may perform substantially all driving functions (e.g., driving, steering, braking, parking, and navigating) without human input. As another example, an autonomous vehicle may be configured to operate without a driver (e.g., the vehicle may be configured to transport human passengers or cargo without a driver present in the vehicle). As another example, an autonomous vehicle may be configured to operate without any human passengers (e.g., the vehicle may be configured for transportation of cargo without having any human passengers onboard the vehicle).
In particular embodiments, an optical signal (which may be referred to as a light signal, a light waveform, an optical waveform, an output beam, or emitted light) may include pulses of light, CW light, amplitude-modulated light, frequency-modulated (FM) light, or any suitable combination thereof. For example, an integrated lidar and radar system 100 as described or illustrated herein may be a pulsed lidar system and may include a light source 110 that produces pulses of light. The pulsed integrated lidar and radar system 100 may include a light source 110 that emits an output light beam 125 with optical pulses having one or more of the following optical characteristics: a wavelength between 900 nm and 2100 nm (e.g., a wavelength of approximately 905 nm, a wavelength between 1500 nm and 1510 nm, a wavelength between 1400 nm and 1600 nm, or any other suitable operating wavelength between 900 nm and 2100 nm); a pulse energy between 0.01 μJ and 100 μJ; a pulse repetition frequency between 80 kHz and 10 MHz; and a pulse duration between 1 ns and 100 ns. For example, the light source 110 in
In particular embodiments, an integrated lidar and radar system 100 may be an FMCW lidar system where the emitted light from the light source 110 (e.g., output light beam 125 in
A light source 110 for an FMCW lidar system may include at least one instance of (i) a direct-emitter laser diode, (ii) a seed laser diode followed by an SOA, (iii) a seed laser diode followed by a fiber-optic amplifier, or (iv) a seed laser diode followed by an SOA and then a fiber-optic amplifier. A seed laser diode or a direct-emitter laser diode may be operated in a CW manner (e.g., by driving the laser diode with a substantially constant DC current), and a frequency modulation may be provided by an external modulator (e.g., an electro-optic phase modulator may apply a frequency modulation to seed-laser light). Alternatively, a frequency modulation may be produced by applying a current modulation to a seed laser diode or a direct-emitter laser diode. The current modulation (which may be provided along with a DC bias current) may produce a corresponding refractive-index modulation in the laser diode, which results in a frequency modulation of the light emitted by the laser diode. The current-modulation component (and the corresponding frequency modulation) may have any suitable frequency or shape (e.g., piecewise linear, sinusoidal, triangle-wave, or sawtooth). For example, the current-modulation component (and the resulting frequency modulation of the emitted light) may increase or decrease monotonically over a particular time interval. As another example, the current-modulation component may include a triangle or sawtooth wave with an electrical current that increases or decreases linearly over a particular time interval, and the light emitted by the laser diode may include a corresponding frequency modulation in which the optical frequency increases or decreases approximately linearly over the particular time interval. For example, a light source 110 that emits light with a linear frequency change of 200 MHz over a 2-μs time interval may be referred to as having a frequency modulation m of 1014 Hz/s (or, 100 MHz/μs).
In addition to producing frequency-modulated emitted light, a light source 110 may also produce frequency-modulated local-oscillator (LO) light. The LO light may be coherent with the emitted light, and the frequency modulation of the LO light may match that of the emitted light. The LO light may be produced by splitting off a portion of the emitted light prior to the emitted light exiting the integrated lidar and radar system 100. Alternatively, the LO light may be produced by a seed laser diode or a direct-emitter laser diode that is part of the light source 110. For example, the LO light may be emitted from the back facet of a seed laser diode or a direct-emitter laser diode, or the LO light may be split off from the seed light emitted from the front facet of a seed laser diode. The received light (e.g., emitted light that is scattered by a target 130) and the LO light may each be frequency modulated, with a frequency difference or offset that corresponds to the distance to the target 130. For a linearly chirped light source (e.g., a frequency modulation that produces a linear change in frequency with time), the larger the frequency difference is between the received light and the LO light, the farther away the target 130 is located.
A frequency difference between received light and LO light may be determined by mixing the received light with the LO light (e.g., by coupling the two beams onto a detector 340 of a light receiver 140 so they are coherently mixed together at the detector) and determining the resulting beat frequency. For example, a photocurrent signal produced by an APD may include a beat signal resulting from the coherent mixing of the received light and the LO light, and a frequency of the beat signal may correspond to the frequency difference between the received light and the LO light. The photocurrent signal from an APD (or a voltage signal that corresponds to the photocurrent signal) may be analyzed using a frequency-analysis technique (e.g., a fast Fourier transform (FFT) technique) to determine the frequency of the beat signal. If a linear frequency modulation m (e.g., in units of Hz/s) is applied to a CW laser, then the round-trip time T may be related to the frequency difference Δf between the received scattered light and the LO light by the expression T=Δf/m. Additionally, the distance D from the target 130 to the integrated lidar and radar system 100 may be expressed as D=(Δf/m)·c/2, where c is the speed of light. For example, for a light source 110 with a linear frequency modulation of 1014 Hz/s, if a frequency difference (between the received scattered light and the LO light) of 33 MHz is measured, then this corresponds to a round-trip time of approximately 330 ns and a distance to the target of approximately 50 meters. As another example, a frequency difference of 133 MHz corresponds to a round-trip time of approximately 1.33 μs and a distance to the target of approximately 200 meters.
In particular embodiments, a receiver or processor of an FMCW lidar system may determine a frequency difference between received scattered light and LO light, and a distance to a target 130 may be determined based on the frequency difference. The frequency difference Δf between received scattered light and LO light corresponds to the round-trip time T (e.g., through the relationship T=Δf/m), and determining the frequency difference may correspond to or may be referred to as determining the round-trip time. For example, a receiver of a FMCW lidar system may determine a frequency difference between received scattered light and LO light, and based on the determined frequency difference, a processor may determine a distance to the target.
In the example of
In particular embodiments, a scan pattern 200 may include multiple pixels 202, and each pixel 202 may be associated with one or more laser pulses or one or more distance measurements. Additionally, a scan pattern 200 may include multiple scan lines 230, where each scan line represents one scan across at least part of a field of regard, and each scan line 230 may include multiple pixels 202. In
In particular embodiments, each pixel 202 may be associated with a distance (e.g., a distance to a portion of a target 130 from which an associated laser pulse was scattered) or one or more angular values. As an example, a pixel 202 may be associated with a distance value and two angular values (e.g., an azimuth and altitude) that represent the angular location of the pixel 202 with respect to the integrated lidar and radar system 100. A distance to a portion of target 130 may be determined based at least in part on a time-of-flight measurement for a corresponding pulse. An angular value (e.g., an azimuth or altitude) may correspond to an angle (e.g., relative to reference line 220) of output light beam 125 (e.g., when a corresponding pulse is emitted from integrated lidar and radar system 100) or an angle of input light beam 135 (e.g., when an input signal is received by integrated lidar and radar system 100). In particular embodiments, an angular value may be determined based at least in part on a position of a component of dual mode scanner 120. As an example, an azimuth or altitude value associated with a pixel 202 may be determined from an angular position of one or more corresponding scanning mirrors of dual mode scanner 120.
In various embodiments, a dual mode scanner 120 may include a polygon mirror 301 configured to scan output light beam 125 along a particular direction. In the example of
In particular embodiments, a polygon mirror 301 may be configured to rotate along a Θx or Θy direction and scan output light beam 125 along a substantially horizontal or vertical direction, respectively. A rotation along a Θx direction may refer to a rotational motion of mirror 301 that results in output light beam 125 scanning along a substantially horizontal direction. Similarly, a rotation along a Θy direction may refer to a rotational motion that results in output light beam 125 scanning along a substantially vertical direction. In
In particular embodiments, a polygon mirror 301 may refer to a multi-sided object having reflective surfaces 320 on two or more of its sides or faces. As an example, a polygon mirror may include any suitable number of reflective faces (e.g., 2, 3, 4, 5, 6, 7, 8, or 10 faces), where each face includes a reflective surface 320. A polygon mirror 301 may have a cross-sectional shape of any suitable polygon, such as for example, a triangle (with three reflecting surfaces 320), square (with four reflecting surfaces 320), pentagon (with five reflecting surfaces 320), hexagon (with six reflecting surfaces 320), heptagon (with seven reflecting surfaces 320), or octagon (with eight reflecting surfaces 320). In
In particular embodiments, a polygon mirror 301 may be continuously rotated in a clockwise or counter-clockwise rotation direction about a rotation axis of the polygon mirror 301. The rotation axis may correspond to a line that is perpendicular to the plane of rotation of the polygon mirror 301 and that passes through the center of mass of the polygon mirror 301. In
In particular embodiments, output light beam 125 may be reflected sequentially from the reflective surfaces 320A, 320B, 320C, and 320D as the polygon mirror 301 is rotated. This results in the output light beam 125 being scanned along a particular scan axis (e.g., a horizontal or vertical scan axis) to produce a sequence of scan lines, where each scan line corresponds to a reflection of the output light beam 125 from one of the reflective surfaces of the polygon mirror 301. In
In particular embodiments, dual mode scanner 120 may be configured to scan both a light-source field of view and a receiver field of view across a field of regard of the integrated lidar and radar system 100. Multiple pulses of light may be emitted and detected as the dual mode scanner 120 scans the FOVL and FOVR across the field of regard of the integrated lidar and radar system 100 while tracing out a scan pattern 200. In particular embodiments, the light-source field of view and the receiver field of view may be scanned synchronously with respect to one another, so that as the FOVL is scanned across a scan pattern 200, the FOVR follows substantially the same path at the same scanning speed. Additionally, the FOVL and FOVR may maintain the same relative position to one another as they are scanned across the field of regard. As an example, the FOVL may be substantially overlapped with or centered inside the FOVR (as illustrated in
In particular embodiments, the FOVL may have an angular size or extent ΘL that is substantially the same as or that corresponds to the divergence of the output light beam 125, and the FOVR may have an angular size or extent ΘR that corresponds to an angle over which the light receiver 140 may receive and detect light. In particular embodiments, the receiver field of view may be any suitable size relative to the light-source field of view. As an example, the receiver field of view may be smaller than, substantially the same size as, or larger than the angular extent of the light-source field of view. In particular embodiments, the light-source field of view may have an angular extent of less than or equal to 50 milliradians, and the receiver field of view may have an angular extent of less than or equal to 50 milliradians. The FOVL may have any suitable angular extent ΘL, such as for example, approximately 0.1 mrad, 0.2 mrad, 0.5 mrad, 1 mrad, 1.5 mrad, 2 mrad, 3 mrad, 5 mrad, 10 mrad, 20 mrad, 40 mrad, or 50 mrad. Similarly, the FOVR may have any suitable angular extent ΘR, such as for example, approximately 0.1 mrad, 0.2 mrad, 0.5 mrad, 1 mrad, 1.5 mrad, 2 mrad, 3 mrad, 5 mrad, 10 mrad, 20 mrad, 40 mrad, or 50 mrad. In particular embodiments, the light-source field of view and the receiver field of view may have approximately equal angular extents. As an example, ΘL and ΘR may both be approximately equal to 1 mrad, 2 mrad, or 4 mrad. In particular embodiments, the receiver field of view may be larger than the light-source field of view, or the light-source field of view may be larger than the receiver field of view. As an example, ΘL may be approximately equal to 3 mrad, and ΘR may be approximately equal to 4 mrad. As another example, ΘR may be approximately K times larger than ΘL, where K is any suitable factor, such as for example, 1.1, 1.2, 1.5, 2, 3, 5, or 10.
In particular embodiments, a pixel 202 may represent or may correspond to a light-source field of view or a receiver field of view. As the output light beam 125 propagates from the light source 110, the diameter of the output light beam 125 (as well as the size of the corresponding pixel 202) may increase according to the beam divergence ΘL. As an example, if the output light beam 125 has a ΘL of 2 mrad, then at a distance of 100 m from the integrated lidar and radar system 100, the output light beam 125 may have a size or diameter of approximately 20 cm, and a corresponding pixel 202 may also have a corresponding size or diameter of approximately 20 cm. At a distance of 200 m from the integrated lidar and radar system 100, the output light beam 125 and the corresponding pixel 202 may each have a diameter of approximately 40 cm.
In particular embodiments, a unidirectional scan pattern 200 may be produced by a dual mode scanner 120 that includes a polygon mirror (e.g., polygon mirror 301 of
In various embodiments, the light receiver 140 includes a detector 340, an amplifier 350, a pulse-detection circuit 365, and a frequency-detection circuit 600. The integrated lidar and radar system 100 illustrated in
In particular embodiments, a coherent pulsed integrated lidar and radar system 100 may include a light source 110 configured to emit pulses of light 400 and LO light 430. The emitted pulses of light 400 may be part of an output light beam 125 that is scanned by a dual mode scanner 120 across a field of regard of the integrated lidar and radar system 100, and the LO light 430 may be sent to a light receiver 140 of the integrated lidar and radar system 100. The light source 110 may include a seed laser that produces seed light and the LO light 430. Additionally, the light source 110 may include an optical amplifier that amplifies the seed light to produce the emitted pulses of light 400. For example, the optical amplifier may be a pulsed optical amplifier that amplifies temporal portions of the seed light to produce the emitted pulses of light 400, where each amplified temporal portion of the seed light corresponds to one of the emitted pulses of light 400. The pulses of light 400 emitted by the light source 110 may have one or more of the following optical characteristics: a wavelength between 900 nm and 1700 nm; a pulse energy between 0.01 μJ and 100 μJ; a pulse repetition frequency between 80 kHz and 10 MHz; and a pulse duration between 0.1 ns and 20 ns. For example, the light source 110 may emit pulses of light 400 with a wavelength of approximately 1550 nm, a pulse energy of approximately 0.5 μJ, a pulse repetition frequency of approximately 750 kHz, and a pulse duration of approximately 5 ns. As another example, the light source 110 may emit pulses of light with a wavelength from approximately 1500 nm to approximately 1510 nm.
In particular embodiments, a coherent pulsed integrated lidar and radar system 100 may include a dual mode scanner 120 configured to scan an output light beam 125 across a field of regard of the integrated lidar and radar system 100. The dual mode scanner 120 may receive the output light beam 125 (which includes the emitted pulses of light 400) from the light source 110, and the dual mode scanner 120 may include one or more scanning mirrors configured to scan the output light beam 125. In addition to scanning the output light beam 125, the scanner may also scan a FOV of the detector 340 across the field of regard so that the output light beam 125 and the detector FOV are scanned synchronously at the same scanning speed or with the same relative position to one another. Alternatively, the integrated lidar and radar system 100 may be configured so that only the output light beam 125 is scanned, and the detector has a static FOV that is not scanned. In this case, the input light beam 135 (which includes received pulses of light 410) may bypass the dual mode scanner 120 and be directed to the light receiver 140 without passing through the dual mode scanner 120.
In particular embodiments, a coherent pulsed integrated lidar and radar system 100 may include an optical combiner 420 configured to optically combine LO light 430 with a received pulse of light 410. Optically combining LO light 430 with a received pulse of light 410 (which is part of the input beam 135) may include spatially overlapping the LO light 430 with the input light beam 135 to produce a combined beam 422. The combined beam 422 may include light from the LO light 430 and the input light beam 135 combined together so that the two beams propagate coaxially along the same path. For example, the combiner 420 in
In particular embodiments, a coherent pulsed integrated lidar and radar system 100 may include a light receiver 140 that detects LO light 430 and received pulses of light 410. A received pulse of light 410 may include light from one of the emitted pulses of light 400 that is scattered by a target 130 located a distance from the integrated lidar and radar system 100. The light receiver 140 may include one or more detectors 340, and the LO light 430 and a received pulse of light 410 may be coherently mixed together at one or more of the detectors 340. One or more of the detectors 340 may produce photocurrent signals that correspond to the coherent mixing of the LO light 430 and the received pulse of light 410. The integrated lidar and radar system 100 in
In particular embodiments, a light receiver 140 may include a pulse-detection circuit 365 that determines a time-of-arrival for a received pulse of light 410. The time-of-arrival for a received pulse of light 410 may correspond to a time associated with a rising edge, falling edge, peak, or temporal center of the received pulse of light 410. The time-of-arrival may be determined based at least in part on a photocurrent signal i produced by a detector 340 of the light receiver 140. For example, a photocurrent signal i may include a pulse of current corresponding to the received pulse of light 410, and the electronic amplifier 350 may produce a voltage signal 360 with a voltage pulse that corresponds to the pulse of current. The pulse-detection circuit 365 may determine the time-of-arrival for the received pulse of light 410 based on a characteristic of the voltage pulse (e.g., based on a time associated with a rising edge, falling edge, peak, or temporal center of the voltage pulse). For example, the pulse-detection circuit 365 may receive an electronic trigger signal (e.g., from the light source 110 or the controller 150) when a pulse of light 400 is emitted, and the pulse-detection circuit 365 may determine the time-of-arrival for the received pulse of light 410 based on a time associated with an edge, peak, or temporal center of the voltage signal 360. The time-of-arrival may be determined based on a difference between a time when the pulse 400 is emitted and a time when the received pulse 410 is detected.
In particular embodiments, a coherent pulsed integrated lidar and radar system 100 may include a processor (e.g., controller 150) that determines the distance to a target 130 based at least in part on a time-of-arrival for a received pulse of light 410. The time-of-arrival for the received pulse of light 410 may correspond to a round-trip time (ΔT) for at least a portion of an emitted pulse of light 400 to travel to the target 130 and back to the integrated lidar and radar system 100, where the portion of the emitted pulse of light 400 that travels back to the target 130 corresponds to the received pulse of light 410. The distance D to the target 130 may be determined from the expression D=c·ΔT/2. For example, if the pulse-detection circuit 365 determines that the time AT between emission of optical pulse 400 and receipt of optical pulse 410 is 1 μs, then the controller 150 may determine that the distance to the target 130 is approximately 150 m. In particular embodiments, a round-trip time may be determined by a light receiver 140, by a controller 150, or by a light receiver 140 and controller 150 together. For example, a light receiver 140 may determine a round-trip time by subtracting a time when a pulse 400 is emitted from a time when a received pulse 410 is detected. As another example, a light receiver 140 may determine a time when a pulse 400 is emitted and a time when a received pulse 410 is detected. These values may be sent to a controller 150, and the controller 150 may determine a round-trip time by subtracting the time when the pulse 400 is emitted from the time when the received pulse 410 is detected.
In particular embodiments, a controller 150 of an integrated lidar and radar system 100 may be coupled to one or more components of the integrated lidar and radar system 100 via one or more data links 425. Each link 425 in
The light receiver 140 illustrated in
In
The pulse-detection circuit 365 in
In particular embodiments, a pulse-detection output signal may be an electrical signal that corresponds to a received pulse of light 410. For example, the pulse-detection output signal in
In particular embodiments, a pulse-detection output signal may include one or more digital values that correspond to a time interval between (1) a time when a pulse of light 400 is emitted and (2) a time when a received pulse of light 410 is detected by a light receiver 140. The pulse-detection output signal in
In
In particular embodiments, a light receiver 140 of an integrated lidar and radar system 100 may include one or more analog-to-digital converters (ADCs). As an example, instead of including multiple comparators and TDCs, a light receiver 140 may include an ADC that receives a voltage signal 360 from amplifier 350 and produces a digital representation of the voltage signal 360. Although this disclosure describes or illustrates example light receivers 140 that include one or more comparators 370 and one or more TDCs 380, a light receiver 140 may additionally or alternatively include one or more ADCs. As an example, in
The example voltage signal 360 illustrated in
In particular embodiments, a pulse-detection output signal produced by a pulse-detection circuit 365 of a light receiver 140 may correspond to or may be used to determine an optical characteristic of a received pulse of light 410 detected by the light receiver 140. An optical characteristic of a received pulse of light 410 may correspond to a peak optical intensity, a peak optical power, an average optical power, an optical energy, a shape or amplitude, a temporal duration, or a temporal center of the received pulse of light 410. For example, a pulse of light 410 detected by light receiver 140 may have one or more of the following optical characteristics: a peak optical power between 1 nanowatt and 10 watts; a pulse energy between 1 attojoule and 10 nanojoules; and a pulse duration between 0.1 ns and 50 ns. In particular embodiments, an optical characteristic of a received pulse of light 410 may be determined from a pulse-detection output signal provided by one or more TDCs 380 of a pulse-detection circuit 365 (e.g., as illustrated in
In particular embodiments, a peak optical power or peak optical intensity of a received pulse of light 410 may be determined from one or more values of a pulse-detection output signal provided by a light receiver 140. As an example, a controller 150 may determine the peak optical power of a received pulse of light 410 based on a peak voltage (Vpeak) of the voltage signal 360. The controller 150 may use a formula or lookup table that correlates a peak voltage of the voltage signal 360 with a value for the peak optical power. In the example of
In particular embodiments, an energy of a received pulse of light 410 may be determined from one or more values of a pulse-detection output signal. For example, a controller 150 may perform a summation of digital values that correspond to a voltage signal 360 to determine an area under the voltage-signal curve, and the area under the voltage-signal curve may be correlated with a pulse energy of a received pulse of light 410. As an example, the approximate area under the voltage-signal curve in
In particular embodiments, a duration of a received pulse of light 410 may be determined from a duration or width of a corresponding voltage signal 360. For example, the difference between two time values of a pulse-detection output signal may be used to determine a duration of a received pulse of light 410. In the example of
In
In particular embodiments, a frequency-detection circuit 600 may include multiple parallel frequency-measurement channels, and each frequency-measurement channel may include a filter 610 and a corresponding amplitude detector 620. In
In addition to the M electronic filters 610, the frequency-detection circuit 600 in
A frequency-detection circuit 600 may include 1, 2, 4, 8, 10, 20, or any other suitable number of filters 610 and amplitude detectors 620, and each filter may have a center frequency between approximately 200 MHz and approximately 20 GHz. Additionally, each filter 610 may include a band-pass filter having a pass-band with a frequency width of approximately 1 MHz, 10 MHz, 20 MHz, 50 MHz, 100 MHz, 200 MHz, or any other suitable frequency width. For example, a frequency-detection circuit 600 may include four band-pass filters 610 with center frequencies of approximately 1.0 GHz, 1.1 GHz, 1.2 GHz, and 1.3 GHz, and each filter may have a pass-band with a frequency width of approximately 20 MHz. A 1.0-GHz filter with a 20-MHz pass-band may pass or transmit frequency components from approximately 0.99 GHz to approximately 1.01 GHz and may attenuate frequency components outside of that frequency range.
In particular embodiments, a light source 110 of an integrated lidar and radar system 100 may impart a particular spectral signature to an emitted pulse of light 400. A spectral signature (which may be referred to as a frequency signature, frequency tag, or frequency change) may correspond to the presence or absence of particular frequency components that are imparted to an emitted pulse of light 400. Additionally or alternatively, a spectral signature may include an amplitude modulation, frequency modulation, or frequency change applied to an emitted pulse of light 400. For example, a spectral signature may include an amplitude or frequency modulation at a particular frequency (e.g., 1 GHz) that is applied to an emitted pulse of light 400. As another example, a spectral signature may include an amplitude or frequency modulation at two or more particular frequencies (e.g., 1.6 GHz and 2.0 GHz) that is applied to an emitted pulse of light 400. A received pulse of light 410 may include the same spectral signature that was applied to an associated emitted pulse of light 400, and the photocurrent signal i (as well as the corresponding voltage signal 360) may include one or more frequency components that correspond to the spectral signature. A frequency-detection circuit 600 may determine, based on the voltage signal 360 (which corresponds to the photocurrent signal i), one or more amplitudes of the one or more frequency components. In the example of
In particular embodiments, a controller 150 may determine, based on the amplitudes of one or more frequency components associated with a received pulse of light 410, whether the received pulse of light 410 is associated with a particular emitted pulse of light 400. If one or more frequency components of a received pulse of light 410 match a spectral signature of a particular emitted pulse of light 400, then the controller 150 may determine that the received pulse of light 410 is associated with the particular emitted pulse of light 400 (e.g., the received pulse of light 410 includes scattered light from the emitted pulse of light 400). Otherwise, if the frequency components do not match, then the controller 150 may determine that the received pulse of light 410 is not associated with the particular emitted pulse of light 400. For example, the received pulse of light 410 may be associated with a different pulse of light 400 emitted by the light source 110 of the integrated lidar and radar system 100, or the received pulse of light 410 may be associated with an interfering optical signal emitted by a different light source external to the integrated lidar and radar system 100. As another example, a particular pulse of light 400 emitted by the light source 110 may include a spectral signature with an amplitude modulation at a particular frequency (e.g., 2 GHz), and a frequency-detection circuit 600 may include a filter 610 and amplitude detector 620 that determine the amplitude of a 2-GHz frequency component for a received pulse of light 410. If the amplitude of the 2-GHz frequency component is greater than a particular threshold value (or within a range of two particular threshold values), then the controller 150 may determine that the received pulse of light 410 is associated with and includes light from the particular emitted pulse of light 400. Otherwise, if the amplitude of the 2-GHz frequency component is less than the particular threshold value, then the controller 150 may determine that the received pulse of light 410 is not associated with and does not include light from the particular emitted pulse of light 400. Additionally or alternatively, if the amplitude of a different frequency component (e.g., a 1.8-GHz frequency component) that is not part of a particular spectral signature is greater than a particular threshold value, then the controller may determine that the received pulse of light 410 is not associated with the emitted pulse of light 400 having that particular spectral signature. In various embodiments, the controller 150 may determine that the received pulse of light 410 is associated with the particular emitted pulse of light 400 based at least in part on correlated radar measurements such as based on a synchronized radio frequency (RF) signal transmitted with the particular emitted pulse of light 400 and a corresponding received reflection of the transmitted RF signal.
In particular embodiments, the amplitudes of the one or more frequency components associated with a received pulse of light 410 may be scaled by a scaling factor. This scaling of the frequency-component amplitudes may be used to compensate for a decrease in the energy, power, or intensity of a received pulse of light 410 as a function of distance of the target 130 from the integrated lidar and radar system 100. A controller 150 may receive, from a frequency-detection circuit 600, digital values corresponding to the amplitudes of one or more frequency components of a received pulse of light 410. Prior to comparing the frequency-component values to threshold values to determine whether the received pulse of light 410 is valid, the frequency-component values may be divided by a scaling factor that corresponds to an optical characteristic of the received pulse of light 410 (e.g., the energy, peak power, or peak intensity of the received pulse of light 410). Alternatively, the frequency-component amplitudes may be multiplied by a scaling factor that corresponds to D or D2, where D is a distance to the target 130 from which the corresponding emitted pulse of light was scattered.
In particular embodiments, a light source 110 may emit pulses of light 400 where each emitted pulse of light 400 has a particular spectral signature of one or more different spectral signatures. The spectral signatures may be used to determine whether a received pulse of light is a valid received pulse of light 410 that is associated with an emitted pulse of light 400. A valid received pulse of light 410 may refer to a received pulse of light 410 that includes scattered light from a pulse of light 400 that was emitted by the light source 110. For example, a light source 110 may emit pulses of light 400 that each include the same spectral signature. If a received pulse of light matches that same spectral signature, then the received pulse of light may be determined to be a valid received pulse of light 410 that is associated with an emitted pulse of light 400. As another example, a light source 110 may emit pulses of light 400 that each include one spectral signature of two or more different spectral signatures. If a received pulse of light matches one of the spectral signatures, then the received pulse of light may be determined to be a valid received pulse of light 410 that is associated with an emitted pulse of light 400.
In particular embodiments, a received pulse of light may be determined to match a particular spectral signature if the received pulse of light includes each of the one or more frequency components associated with the particular spectral signature. Additionally, a received pulse of light may be determined to match the particular spectral signature if the received pulse of light does not include any frequency components that are not associated with the particular spectral signature. Similarly, a received pulse of light may be determined to not match a spectral signature if (i) the received pulse of light does not include all of the one or more frequency components associated with the spectral signature or (ii) the received pulse of light includes one or more frequency components not associated with the spectral signature. Determining whether a received pulse of light 410 includes a particular frequency component may include determining the amplitude of the particular frequency component (e.g., based on a signal from an amplitude detector 620). If the amplitude of the particular frequency component is greater than a particular threshold value (or between a minimum threshold value and a maximum threshold value), then a controller 150 may determine that a received pulse of light 410 includes the particular frequency component. Additionally or alternatively, if the amplitude of the particular frequency component is less than the particular threshold value, then the controller 150 may determine that the received pulse of light 410 does not include the particular frequency component.
In particular embodiments, a light source 110 may emit pulses of light 400 where each emitted pulse of light 400 has a particular spectral signature of two or more different spectral signatures, and the spectral signatures may be used to associate a received pulse of light 410 with a particular emitted pulse of light 400. For example, a light source 110 may emit pulses of light 400 with spectral signatures that alternate (e.g., sequentially or in a pseudo-random manner) between two, three, four, or any other suitable number of different spectral signatures. One spectral signature may include an amplitude modulation at 1.5 GHz, and another spectral signature may include an amplitude modulation at 1.7 GHz. A frequency-detection circuit 600 may include two filters and amplitude detectors that determine the amplitudes of the frequency components at 1.5 GHz and 1.7 GHz. Based on the amplitudes of the 1.5-GHz and 1.7-GHz frequency components of a received pulse of light 410, the controller 150 may determine whether the received pulse of light 410 is associated with an emitted pulse of light 400 having a 1.5-GHz spectral signature or a 1.7-GHz spectral signature. If a light source 110 emits a first pulse with a 1.5-GHz modulation and a second pulse with a 1.7-GHz modulation, then a controller 150 may determine that a received pulse of light 410 with a 1.5-GHz frequency component is associated with the first emitted pulse. Emitting pulses of light 400 that have different spectral signatures may allow a frequency-detection circuit 600 and controller 150 to prevent problems with ambiguity as to which emitted pulse a received pulse is associated with. A received pulse of light 410 may be unambiguously associated with an emitted pulse of light 400 based on the frequency components of the received pulse of light 410 matching the spectral signature of the emitted pulse of light 400.
In particular embodiments, a light source 110 may emit pulses of light 400 where each emitted pulse of light 400 has a particular spectral signature of one or more different spectral signatures, and the spectral signatures may be used to determine whether a received pulse of light is a valid received pulse of light 410 or an interfering optical signal. An interfering optical signal may refer to an optical signal that is sent by a light source external to the integrated lidar and radar system 100. For example, another lidar system or integrated lidar and radar system may emit a pulse of light that is detected by the light receiver 140, and the received pulse of light may be determined to be an interfering optical signal since it does not match the spectral signatures of the emitted pulses of light 400 from the light source 110. A controller 150 may distinguish valid pulses from interfering pulses by comparing the frequency components for a received pulse of light with the expected frequency components associated with the spectral signatures imparted to emitted pulses of light 400. If the frequency components of a received pulse of light do not match any of the one or more different spectral signatures imparted to the emitted pulses of light 400, then the controller 150 may determine that the received pulse of light is invalid and is not associated with any of the emitted pulses of light 400. For example, the received pulse of light may be an interfering pulse of light sent from a light source external to the integrated lidar and radar system 100, and the interfering pulse of light may be discarded or ignored since it is not associated with any of the emitted pulses of light 400.
The embodiment of dual mode scanner 120 illustrates a configuration where light source 110 and radio frequency (RF) source 210 are positioned such that their corresponding emitted light pulses and radio frequency (RF) signals reflect off different surfaces of polygon mirror 301. As shown
In some embodiments, polygon mirror 301 and scan mirror 302 include materials that are reflective for both light and radio frequency (RF) signals. For example, polygon mirror 301 and scan mirror 302 may be one or more metals that can reflect both light and RF signals. In some embodiments, polygon mirror 301 and scan mirror 302 may each be coated, for example, with a protective layer such as gold. A protective layer allows polygon mirror 301 and scan mirror 302 to reflect both light and RF signals while also protecting the mirrors from effects such as oxidation.
The embodiment of dual mode scanner 120 in
In particular embodiments, by utilizing polygon mirror 301 that is reflective for both light and radio frequency (RF) signals, output light beam 125 and output radio frequency (RF) signal 225 can be coordinated and synchronized along the Θx direction. With a material transmissive to RF signals, scan mirror 302 allows output light beam 125 to be decoupled from output RF signal 225 along the Θy direction. In various embodiments, the Θx and Θy directions corresponding to polygon mirror 301 and scan mirror 302, respectively, are example directions and another coordinate system may be appropriate as well. In some embodiments, the Θx and Oy directions may be orthogonal or non-orthogonal to one another. Although utilizing different facets of polygon mirror 301, based on the placement and calibration of light source 110 and RF source 210 relative to polygon mirror 301, dual mode scanner 120 can be configured to scan different and/or overlapping regions of interest for both light pulses and RF signals.
In some embodiments, polygon mirror 301 includes materials that are reflective for both light and radio frequency (RF) signals and scan mirror 302 utilizes materials that are reflective to light but transmissive to RF signals. For example, an optical coating of scan mirror 302 can allow for different scan functions by reflecting light pulses while sufficiently transmitting RF signals. In some embodiments, scan mirror 302 is a dichroic mirror that reflects light but is transmissive to radar wavelengths.
In various embodiments, the arrangement of the lidar and radar components including the two mirrors, polygon mirror 301 and scan mirror 302, as shown in
The embodiment of dual mode scanner 120 illustrates a configuration where light source 110 and radio frequency (RF) source 210 are positioned such that their corresponding emitted light pulses and radio frequency (RF) signals are combined using beam combiner 250 and both reflect off the same surface of polygon mirror 301. As illustrated, polygon mirror 301 is configured to rotate along a Θx direction and simultaneously scan output light beam 125 and output radio frequency (RF) signal 225 along a substantially horizontal direction at scan mirror 302. Scan mirror 302 is configured to rotate along a Θy direction and simultaneously scan output light beam 125 and output radio frequency (RF) signal 225 along a substantially vertical direction. In some embodiments, polygon mirror 301 is an azimuth mirror and scan mirror 302 is an elevation mirror. By utilizing both polygon mirror 301 and scan mirror 302, output light beam 125 and output RF signal 225 can be directed along both a Θx direction and a Θy direction to manipulate their azimuth and elevation, respectively and independently. In various embodiments, the Θx and Θy directions corresponding to polygon mirror 301 and scan mirror 302, respectively, are example directions and another coordinate system may be appropriate as well. In some embodiments, the Θx and Θy directions may be orthogonal or non-orthogonal to one another. By combining emitted output light beam 125 and transmitted output RF signal 225 together and utilizing the same facet of polygon mirror 301, dual mode scanner 120 can be configured to scan the same region of interest for both light pulses and RF signals, directing output light beam 125 and output RF signal 225 along coordinated and/or synchronized paths.
Although not shown in
In some embodiments, mirror component 303 is a portion of a mirror of a dual mode scanner and one or more instances of mirror component 303 can be included in a single mirror. In some embodiments, one or more instances of mirror component 303 may be incorporated in any of the mirrors including polygon and scan mirrors of
In some embodiments, surface A of mirror component 303 is implemented as an optical coating that reflects optical beams but sufficiently transmits radar. Surface B can be implemented as a curved metallic surface. The different surfaces allow for focusing and/or modifying the corresponding reflected beam. For example, surface B can be shaped to focus and/or modify the divergence of a received radio frequency (RF) signal. In some embodiments, a radio frequency (RF) source component such as RF source 210 of
In some embodiments, mirror component 303 is part of a dichroic mirror. For example, surface A of mirror component 303 can include a dichroic coating and the surface B can include a metallic coating. In some embodiments, mirror component 303 is constructed at least in part of a plastic or glass material. For example, the material between surfaces A and B can be a glass material or glass substrate with a dichroic coating for surface A and a metallic surface of a specific thickness for surface B. The material of surface B may be gold, aluminum, or another material reflective for radio frequency (RF) signals.
In some embodiments, integrated lidar and radar system 100 of
In various embodiments, with a hybrid approach, the transmitting and receiving of the RF signals can be performed from two (or more) different locations. For example, the transmitting of RF signals can be performed via a mirror assembly of integrated lidar and radar system 100 and mechanically scanned in sync with corresponding light pulses using dual mode scanner 120. However, the received RF signals can be received from one (or more) receiving antennas located at one or more different physical locations from dual mode scanner 120. In a hybrid approach, the transmission and receiving components for RF signals need not be co-located, allowing for customized applications and the use of multi-location antenna receivers.
Computer system 1300 may take any suitable physical form. As an example, computer system 1300 may be an embedded computer system, a system-on-chip (SOC), a single-board computer system (SBC), a desktop computer system, a laptop or notebook computer system, a mainframe, a mesh of computer systems, a server, a tablet computer system, or any suitable combination of two or more of these. As another example, all or part of computer system 1300 may be combined with, coupled to, or integrated into a variety of devices, including, but not limited to, a camera, camcorder, personal digital assistant (PDA), mobile telephone, smartphone, electronic reading device (e.g., an e-reader), game console, smart watch, clock, calculator, television monitor, flat-panel display, computer monitor, vehicle display (e.g., odometer display or dashboard display), vehicle navigation system, lidar system, integrated lidar and radar system, ADAS, autonomous vehicle, autonomous-vehicle driving system, cockpit control, camera view display (e.g., display of a rear-view camera in a vehicle), eyewear, or head-mounted display. Where appropriate, computer system 1300 may include one or more computer systems 1300; be unitary or distributed; span multiple locations; span multiple machines; span multiple data centers; or reside in a cloud, which may include one or more cloud components in one or more networks. Where appropriate, one or more computer systems 1300 may perform without substantial spatial or temporal limitation one or more steps of one or more methods described or illustrated herein. As an example, one or more computer systems 1300 may perform in real time or in batch mode one or more steps of one or more methods described or illustrated herein. One or more computer systems 1300 may perform at different times or at different locations one or more steps of one or more methods described or illustrated herein, where appropriate.
As illustrated in the example of
In particular embodiments, processor 1310 may include hardware for executing instructions, such as those making up a computer program. As an example, to execute instructions, processor 1310 may retrieve (or fetch) the instructions from an internal register, an internal cache, memory 1320, or storage 1330; decode and execute them; and then write one or more results to an internal register, an internal cache, memory 1320, or storage 1330. In particular embodiments, processor 1310 may include one or more internal caches for data, instructions, or addresses. Processor 1310 may include any suitable number of any suitable internal caches, where appropriate. As an example, processor 1310 may include one or more instruction caches, one or more data caches, or one or more translation lookaside buffers (TLBs). Instructions in the instruction caches may be copies of instructions in memory 1320 or storage 1330, and the instruction caches may speed up retrieval of those instructions by processor 1310. Data in the data caches may be copies of data in memory 1320 or storage 1330 for instructions executing at processor 1310 to operate on; the results of previous instructions executed at processor 1310 for access by subsequent instructions executing at processor 1310 or for writing to memory 1320 or storage 1330; or other suitable data. The data caches may speed up read or write operations by processor 1310. The TLBs may speed up virtual-address translation for processor 1310. In particular embodiments, processor 1310 may include one or more internal registers for data, instructions, or addresses. Processor 1310 may include any suitable number of any suitable internal registers, where appropriate. Where appropriate, processor 1310 may include one or more arithmetic logic units (ALUs); may be a multi-core processor; or may include one or more processors 1310.
In particular embodiments, memory 1320 may include main memory for storing instructions for processor 1310 to execute or data for processor 1310 to operate on. As an example, computer system 1300 may load instructions from storage 1330 or another source (such as, for example, another computer system 1300) to memory 1320. Processor 1310 may then load the instructions from memory 1320 to an internal register or internal cache. To execute the instructions, processor 1310 may retrieve the instructions from the internal register or internal cache and decode them. During or after execution of the instructions, processor 1310 may write one or more results (which may be intermediate or final results) to the internal register or internal cache. Processor 1310 may then write one or more of those results to memory 1320. One or more memory buses (which may each include an address bus and a data bus) may couple processor 1310 to memory 1320. Bus 1360 may include one or more memory buses. In particular embodiments, one or more memory management units (MMUs) may reside between processor 1310 and memory 1320 and facilitate accesses to memory 1320 requested by processor 1310. In particular embodiments, memory 1320 may include random access memory (RAM). This RAM may be volatile memory, where appropriate. Where appropriate, this RAM may be dynamic RAM (DRAM) or static RAM (SRAM). Memory 1320 may include one or more memories 1320, where appropriate.
In particular embodiments, storage 1330 may include mass storage for data or instructions. As an example, storage 1330 may include a hard disk drive (HDD), a floppy disk drive, flash memory, an optical disc, a magneto-optical disc, magnetic tape, or a Universal Serial Bus (USB) drive or a combination of two or more of these. Storage 1330 may include removable or non-removable (or fixed) media, where appropriate. Storage 1330 may be internal or external to computer system 1300, where appropriate. In particular embodiments, storage 1330 may be non-volatile, solid-state memory. In particular embodiments, storage 1330 may include read-only memory (ROM). Where appropriate, this ROM may be mask ROM (MROM), programmable ROM (PROM), erasable PROM (EPROM), electrically erasable PROM (EEPROM), flash memory, or a combination of two or more of these. Storage 1330 may include one or more storage control units facilitating communication between processor 1310 and storage 1330, where appropriate. Where appropriate, storage 1330 may include one or more storages 1330.
In particular embodiments, I/O interface 1340 may include hardware, software, or both, providing one or more interfaces for communication between computer system 1300 and one or more I/O devices. Computer system 1300 may include one or more of these I/O devices, where appropriate. One or more of these I/O devices may enable communication between a person and computer system 1300. As an example, an I/O device may include a keyboard, keypad, microphone, monitor, mouse, printer, scanner, speaker, camera, stylus, tablet, touch screen, trackball, another suitable I/O device, or any suitable combination of two or more of these. An I/O device may include one or more sensors. Where appropriate, I/O interface 1340 may include one or more device or software drivers enabling processor 1310 to drive one or more of these I/O devices. I/O interface 1340 may include one or more I/O interfaces 1340, where appropriate.
In particular embodiments, communication interface 1350 may include hardware, software, or both providing one or more interfaces for communication (such as, for example, packet-based communication) between computer system 1300 and one or more other computer systems 1300 or one or more networks. As an example, communication interface 1350 may include a network interface controller (NIC) or network adapter for communicating with an Ethernet or other wire-based network or a wireless NIC (WNIC); a wireless adapter for communicating with a wireless network, such as a WI-FI network; or an optical transmitter (e.g., a laser or a light-emitting diode) or an optical receiver (e.g., a photodetector) for communicating using fiber-optic communication or free-space optical communication. Computer system 1300 may communicate with an ad hoc network, a personal area network (PAN), an in-vehicle network (IVN), a local area network (LAN), a wide area network (WAN), a metropolitan area network (MAN), or one or more portions of the Internet or a combination of two or more of these. One or more portions of one or more of these networks may be wired or wireless. As an example, computer system 1300 may communicate with a wireless PAN (WPAN) (such as, for example, a BLUETOOTH WPAN), a WI-FI network, a Worldwide Interoperability for Microwave Access (WiMAX) network, a cellular telephone network (such as, for example, a Global System for Mobile Communications (GSM) network), or other suitable wireless network or a combination of two or more of these. As another example, computer system 1300 may communicate using fiber-optic communication based on 100 Gigabit Ethernet (100 GbE), 10 Gigabit Ethernet (10 GbE), or Synchronous Optical Networking (SONET). Computer system 1300 may include any suitable communication interface 1350 for any of these networks, where appropriate. Communication interface 1350 may include one or more communication interfaces 1350, where appropriate.
In particular embodiments, bus 1360 may include hardware, software, or both coupling components of computer system 1300 to each other. As an example, bus 1360 may include an Accelerated Graphics Port (AGP) or other graphics bus, a controller area network (CAN) bus, an Enhanced Industry Standard Architecture (EISA) bus, a front-side bus (FSB), a HYPERTRANSPORT (HT) interconnect, an Industry Standard Architecture (ISA) bus, an INFINIBAND interconnect, a low-pin-count (LPC) bus, a memory bus, a Micro Channel Architecture (MCA) bus, a Peripheral Component Interconnect (PCI) bus, a PCI-Express (PCIe) bus, a serial advanced technology attachment (SATA) bus, a Video Electronics Standards Association local bus (VLB), or another suitable bus or a combination of two or more of these. Bus 1360 may include one or more buses 1360, where appropriate.
In particular embodiments, various modules, circuits, systems, methods, or algorithm steps described in connection with the implementations disclosed herein may be implemented as electronic hardware, computer software, or any suitable combination of hardware and software. In particular embodiments, computer software (which may be referred to as software, computer-executable code, computer code, a computer program, computer instructions, or instructions) may be used to perform various functions described or illustrated herein, and computer software may be configured to be executed by or to control the operation of computer system 1300. As an example, computer software may include instructions configured to be executed by processor 1310. In particular embodiments, owing to the interchangeability of hardware and software, the various illustrative logical blocks, modules, circuits, or algorithm steps have been described generally in terms of functionality. Whether such functionality is implemented in hardware, software, or a combination of hardware and software may depend upon the particular application or design constraints imposed on the overall system.
In particular embodiments, a computing device may be used to implement various modules, circuits, systems, methods, or algorithm steps disclosed herein. As an example, all or part of a module, circuit, system, method, or algorithm disclosed herein may be implemented or performed by a general-purpose single- or multi-chip processor, a digital signal processor (DSP), an ASIC, a FPGA, any other suitable programmable-logic device, discrete gate or transistor logic, discrete hardware components, or any suitable combination thereof. A general-purpose processor may be a microprocessor, or, any conventional processor, controller, microcontroller, or state machine. A processor may also be implemented as a combination of computing devices, e.g., a combination of a DSP and a microprocessor, a plurality of microprocessors, one or more microprocessors in conjunction with a DSP core, or any other such configuration.
In particular embodiments, one or more implementations of the subject matter described herein may be implemented as one or more computer programs (e.g., one or more modules of computer-program instructions encoded or stored on a computer-readable non-transitory storage medium). As an example, the steps of a method or algorithm disclosed herein may be implemented in a processor-executable software module which may reside on a computer-readable non-transitory storage medium. In particular embodiments, a computer-readable non-transitory storage medium may include any suitable storage medium that may be used to store or transfer computer software and that may be accessed by a computer system. Herein, a computer-readable non-transitory storage medium or media may include one or more semiconductor-based or other integrated circuits (ICs) (such, as for example, field-programmable gate arrays (FPGAs) or application-specific ICs (ASICs)), hard disk drives (HDDs), hybrid hard drives (HHDs), optical discs (e.g., compact discs (CDs), CD-ROM, digital versatile discs (DVDs), blu-ray discs, or laser discs), optical disc drives (ODDs), magneto-optical discs, magneto-optical drives, floppy diskettes, floppy disk drives (FDDs), magnetic tapes, flash memories, solid-state drives (SSDs), RAM, RAM-drives, ROM, SECURE DIGITAL cards or drives, any other suitable computer-readable non-transitory storage media, or any suitable combination of two or more of these, where appropriate. A computer-readable non-transitory storage medium may be volatile, non-volatile, or a combination of volatile and non-volatile, where appropriate.
In particular embodiments, certain features described herein in the context of separate implementations may also be combined and implemented in a single implementation. Conversely, various features that are described in the context of a single implementation may also be implemented in multiple implementations separately or in any suitable sub-combination. Moreover, although features may be described above as acting in certain combinations and even initially claimed as such, one or more features from a claimed combination may in some cases be excised from the combination, and the claimed combination may be directed to a sub-combination or variations of a sub-combination.
While operations may be depicted in the drawings as occurring in a particular order, this should not be understood as requiring that such operations be performed in the particular order shown or in sequential order, or that all operations be performed. Further, the drawings may schematically depict one more example processes or methods in the form of a flow diagram or a sequence diagram. However, other operations that are not depicted may be incorporated in the example processes or methods that are schematically illustrated. For example, one or more additional operations may be performed before, after, simultaneously with, or between any of the illustrated operations. Moreover, one or more operations depicted in a diagram may be repeated, where appropriate. Additionally, operations depicted in a diagram may be performed in any suitable order. Furthermore, although particular components, devices, or systems are described herein as carrying out particular operations, any suitable combination of any suitable components, devices, or systems may be used to carry out any suitable operation or combination of operations. In certain circumstances, multitasking or parallel processing operations may be performed. Moreover, the separation of various system components in the implementations described herein should not be understood as requiring such separation in all implementations, and it should be understood that the described program components and systems may be integrated together in a single software product or packaged into multiple software products.
Various embodiments have been described in connection with the accompanying drawings. However, it should be understood that the figures may not necessarily be drawn to scale. As an example, distances or angles depicted in the figures are illustrative and may not necessarily bear an exact relationship to actual dimensions or layouts of the devices illustrated.
The scope of this disclosure encompasses all changes, substitutions, variations, alterations, and modifications to the example embodiments described or illustrated herein that a person having ordinary skill in the art would comprehend. The scope of this disclosure is not limited to the example embodiments described or illustrated herein. Moreover, although this disclosure describes or illustrates respective embodiments herein as including particular components, elements, functions, operations, or steps, any of these embodiments may include any combination or permutation of any of the components, elements, functions, operations, or steps described or illustrated anywhere herein that a person having ordinary skill in the art would comprehend.
The term “or” as used herein is to be interpreted as an inclusive or meaning any one or any combination, unless expressly indicated otherwise or indicated otherwise by context. Therefore, herein, the expression “A or B” means “A, B, or both A and B.” As another example, herein, “A, B or C” means at least one of the following: A; B; C; A and B; A and C; B and C; A, B and C. An exception to this definition will occur if a combination of elements, devices, steps, or operations is in some way inherently mutually exclusive.
As used herein, words of approximation such as, without limitation, “approximately, “substantially,” or “about” refer to a condition that when so modified is understood to not necessarily be absolute or perfect but would be considered close enough to those of ordinary skill in the art to warrant designating the condition as being present. The extent to which the description may vary will depend on how great a change can be instituted and still have one of ordinary skill in the art recognize the modified feature as having the required characteristics or capabilities of the unmodified feature. In general, but subject to the preceding discussion, a numerical value herein that is modified by a word of approximation such as “approximately” may vary from the stated value by ±0.5%, ±1%, ±2%, 3%, ±4%, ±5%, ±10%, ±12%, or ±15%. The term “substantially constant” refers to a value that varies by less than a particular amount over any suitable time interval. For example, a value that is substantially constant may vary by less than or equal to 20%, 10%, 1%, 0.5%, or 0.1% over a time interval of approximately 104 s, 103 s, 102 s, 10 s, 1 s, 100 ms, 10 ms, 1 ms, 100 μs, 10 μs, or 1 μs. The term “substantially constant” may be applied to any suitable value, such as for example, an optical power, a pulse repetition frequency, an electrical current, a wavelength, an optical or electrical frequency, or an optical or electrical phase.
As used herein, the terms “first,” “second,” “third,” etc. may be used as labels for nouns that they precede, and these terms may not necessarily imply a particular ordering (e.g., a particular spatial, temporal, or logical ordering). As an example, a system may be described as determining a “first result” and a “second result,” and the terms “first” and “second” may not necessarily imply that the first result is determined before the second result.
As used herein, the terms “based on” and “based at least in part on” may be used to describe or present one or more factors that affect a determination, and these terms may not exclude additional factors that may affect a determination. A determination may be based solely on those factors which are presented or may be based at least in part on those factors. The phrase “determine A based on B” indicates that B is a factor that affects the determination of A. In some instances, other factors may also contribute to the determination of A. In other instances, A may be determined based solely on B.
Although the foregoing embodiments have been described in some detail for purposes of clarity of understanding, the invention is not limited to the details provided. There are many alternative ways of implementing the invention. The disclosed embodiments are illustrative and not restrictive.
This application claims priority to U.S. Provisional Patent Application No. 63/610,763 entitled INTEGRATED LIDAR AND RADAR SYSTEM filed Dec. 15, 2023 which is incorporated herein by reference for all purposes.
| Number | Date | Country | |
|---|---|---|---|
| 63610763 | Dec 2023 | US |
