Patent Application
20250093488
This invention relates to operation of a radar system, and more particularly, to detecting change in position of objects within a field of view of a radar system.
Generally, in radar systems, such as Doppler radar systems, a set of emitted electromagnetic (EM) pulses may strike an object in a field of view (FOV) of the radar system and be reflected. A receiver of the radar system may receive a set of reflected EM pulses. If the object has a velocity relative to the radar system, the set of reflected EM pulses may be shifted by the Doppler effect, relative the set of emitted EM pulses. The Doppler effect may be used to determine the relative velocity of the object.
However, in some instances, a stationary object may be large, and may be placed such that it partially or completely occludes the FOV of the radar system. Further, in some other instances, in the event that a small object may be placed close to the receiver to partially or fully occlude receiver. At this juncture, the radar system may not be able to determine if any movement is occurring behind the object.
In an example, the radar system (such as the Doppler radar system) may be used for purposes of security in a FOV. The radar system may detect movement into and out of the FOV but may not register if an object within the FOV was newly placed, or moved a little.
Disclosed herein is a radar system configured with a range gating mechanism. The radar system includes a transmitter configured to emit a set of electromagnetic pulses in a region defining a field of view (FOV) of the radar system. The radar system further includes a receiver configured to detect a set of reflected electromagnetic pulses originating responsive to reflection of the set of emitted electromagnetic pulses from an object located within the FOV of the radar system. The radar system further includes a modulator communicably coupled to the transmitter and configured to selectively append a modulated signal to the set of emitted electromagnetic pulses. The radar system further includes a computing device communicably coupled to the transmitter, the receiver, and the modulator. The computing device is configured to determine one or more first pulse attributes related to a first set of reflected electromagnetic pulses during a first period of time. The computing device is further configured to operate the modulator to append a modulated signal to the set of emitted electromagnetic pulses. The computing device is further configured to determine one or more second pulse attributes related to a second set of reflected electromagnetic pulses during a second period of time. The computing device is further configured to determine, based on the one or more first and second pulse attributes, a change of position of the object within the FOV of the radar system during a period between the first period of time and the second period of time.
In one or more embodiments, the computing device is configured to intermittently operate the modulator to append the modulated signal to the set of emitted electromagnetic pulses.
In one or more embodiments, the computing device is configured to operate the modulator to continuously append the modulated signal to the set of emitted electromagnetic pulses.
In one or more embodiments, the one or more pulse attributes include one or more of an amplitude of the set of reflected electromagnetic pulses, and a phase difference between the corresponding set of emitted electromagnetic pulses and the set of reflected electromagnetic pulses.
In one or more embodiments, the computing device is further configured to determine, a first amplitude of the first set of reflected electromagnetic pulses. The computing device is further configured to determine a second amplitude of the second set of reflected electromagnetic pulses. The computing device is further configured to determine the change in position of the object based on the first and second amplitudes.
In one or more embodiments, the modulated signal is a frequency modulated signal.
In one or more embodiments, the first and second sets of reflected electromagnetic pulses are transformed in frequency domain using any one or a combination of filtering, convolution, and autocorrelation.
In one or more embodiments, the computing device is configured to operate the modulator to append the modulated signal to the set of emitted electromagnetic pulses during any one period of time, such that the modulated signal during the any one period of time includes at least first and second frequencies different from each other.
In one or more embodiments, the first and second sets of reflected electromagnetic pulses are filtered in the frequency domain, and wherein a frequency difference of the modulated signal is in a passband.
Further disclosed herein is a method for a radar system configured with a range gating mechanism. The method includes determining, by a computing device, one or more first pulse attributes related to a first set of reflected electromagnetic pulses during a first period of time. The method further includes operating, by the computing device, a modulator to append a modulated signal to a set of emitted electromagnetic pulses. The method further includes determining, by the computing device, one or more second pulse attributes related to a second set of reflected electromagnetic pulses during a second period of time. The method further includes determining, by the computing device, based on the one or more first and second pulse attributes, a change of position of the object within the FOV of the radar system during a period between the first period of time and the second period of time.
In one or more embodiments, the method includes operating intermittently, by the computing device, the modulator to append the modulated signal to the set of emitted electromagnetic pulses.
In one or more embodiments, the method includes operating, by the computing device, the modulator to continuously append the modulated signal to the set of emitted electromagnetic pulses.
In one or more embodiments, the one or more pulse attributes includes one or more of an amplitude of the set of reflected electromagnetic pulses, and a phase difference between the corresponding set of emitted electromagnetic pulses and the set of reflected electromagnetic pulses.
In one or more embodiments, the method further includes determining, by the computing device, a first amplitude of the first set of reflected electromagnetic pulses. The method further includes determining, by the computing device, a second amplitude of the second set of reflected electromagnetic pulses. The method further includes determining, by the computing device, the change in position of the object based on the first and second amplitudes.
In one or more embodiments, the modulated signal is a frequency modulated signal.
In one or more embodiments, the first and second sets of reflected electromagnetic pulses are transformed in frequency domain using any one or a combination of filtering, convolution, and autocorrelation.
In one or more embodiments, the method further includes operating, by the computing device, the modulator to append the modulated signal to the set of emitted electromagnetic pulses during any one period of time, such that the modulated signal during the any one period of time includes at least first and second frequencies different from each other.
In one or more embodiments, the first and second sets of reflected electromagnetic pulses are filtered in the frequency domain, and wherein a frequency difference of the modulated signal is in a passband.
The foregoing summary is illustrative only and is not intended to be in any way limiting. In addition to the illustrative aspects, embodiments, and features described above, further aspects, embodiments, features, and techniques of the invention will become more apparent from the following description taken in conjunction with the drawings.
The accompanying drawings are included to provide a further understanding of the subject disclosure of this invention and are incorporated in and constitute a part of this specification. The drawings illustrate exemplary embodiments of the subject disclosure and, together with the description, serve to explain the principles of the subject disclosure.
In the drawings, similar components and/or features may have the same reference label. Further, various components of the same type may be distinguished by following the reference label with a second label that distinguishes among the similar components. If only the first reference label is used in the specification, the description is applicable to any one of the similar components having the same first reference label irrespective of the second reference label.
The following is a detailed description of embodiments of the disclosure depicted in the accompanying drawings. The embodiments are in such detail as to clearly communicate the disclosure. However, the amount of detail offered is not intended to limit the anticipated variations of embodiments; on the contrary, the intention is to cover all modifications, equivalents, and alternatives falling within the spirit and scope of the subject disclosure as defined by the appended claims.
Various terms are used herein. To the extent a term used in a claim is not defined below, it should be given the broadest definition persons in the pertinent art have given that term as reflected in printed publications and issued patents at the time of filing.
In the specification, reference may be made to the spatial relationships between various components and to the spatial orientation of various aspects of components as the devices are depicted in the attached drawings. However, as will be recognized by those skilled in the art after a complete reading of the subject disclosure, the components of this invention. described herein may be positioned in any desired orientation. Thus, the use of terms such as “above,” “below,” “upper,” “lower,” “first”, “second” or other like terms to describe a spatial relationship between various components or to describe the spatial orientation of aspects of such components should be understood to describe a relative relationship between the components or a spatial orientation of aspects of such components.
Referring to
In one or more embodiments, the radar system 100 may be a Doppler radar system. Generally, a set of emitted EM pulses may strike an object in a FOV of the radar system and be reflected. A receiver of the radar system may receive the set of reflected EM pulses. If the object has a velocity relative to the radar system, the set of reflected EM pulses is shifted by the Doppler effect, relative the set of emitted EM pulses. The Doppler effect may be used to determine the relative velocity of the object.
However, in some instances, a stationary object may be large, and may be placed, such that it partially or completely occludes the FOV of the radar system. Further, in some other instances, in the event that a small object may be placed close to the receiver to partially or fully occlude receiver. At this juncture, the radar system may not be able to determine if any movement is occurring behind the object.
In an example, the radar system (such as the Doppler radar system) may be used for purposes of security in a FOV. The radar system may detect movement into and out of the FOV but may not register if an object within the FOV was newly placed, or moved a little.
Thus, there is a requirement for a means to determine, using the radar system, presence or relocation of an object, and location or distance of the object relative to the radar system. Further, preferably, the means may be cost effective, and be capable of being integrated into existing radar systems without a requirement for significant modifications of the existing radar systems.
In continued reference to
The radar system 100 may further include a signal processing unit 112 communicably coupled to the transmitter 102, the receiver 104, and the modulator 110. The signal processing unit 112 may be configured to receive signals generated by the receiver 104 over a plurality of successive periods of time. The signal processing unit 112 may be further configured to generate corresponding electric voltages in response to received signals. In one or more embodiments, the electric voltages are direct current (DC) voltages. In some other embodiments, the electric voltages are alternating current (AC) voltages. The generated electric voltages may have a magnitude that is based on one or more pulse attributes of the respective received signals from the receiver 104. In one or more embodiments, the one or more pulse attributes may include one or more of an amplitude of the set of reflected EM pulses, and a phase difference between the corresponding set of emitted EM pulses and the set of reflected EM pulses. In one or more embodiments, the one or more pulse attributes may be indicative of a distance of the object 190 from the radar system 100.
The radar system 100 further includes a computing device 200. The computing device 200 may be configured for operating the radar system 100. The computing device 200 may be implemented by way of a single device or a combination of multiple devices that may be communicably coupled or networked together. The computing device 200 may be implemented in hardware or a suitable combination of hardware and software. The computing device 200 may be a hardware device including a processor executing machine-readable program instructions. The “hardware” may include a combination of discrete components, an integrated circuit, an application-specific integrated circuit, a field programmable gate array, a digital signal processor, or other suitable hardware. The “software” may include one or more objects, agents, threads, lines of code, subroutines, separate software applications, two or more lines of code or other suitable software structures operating in one or more software applications or on one or more processors. The processor may include, for example, without limitations, microprocessors, microcomputers, microcontrollers, digital signal processors, central processing units, state machines, logic circuits, any devices that manipulate data or signals based on operational instructions, and the like. Among other capabilities, the processor may fetch and execute computer-readable instructions in the memory operationally coupled with the computing device 200 for performing tasks such as data processing, input/output processing, feature extraction, and/or any other functions. Any reference to a task in the present disclosure may refer to an operation being or that may be performed on data.
The radar system 100 may further include units, such as, without limitations, a display unit, an audio unit, a notification unit, an input unit, an output unit, and the like; however, the same are not shown in the
Referring to
Referring now to
The processing engine 210 may include a pulse attributes engine 212, modulator operation engine 214, an object location determination engine 216, and other engine(s) 218. The other engine(s) 218 may include engines configured to perform one or more functions ancillary functions associated with the processing engine 210.
The pulse attributes engine 212 may be configured to determine one or more first pulse attributes related to a first set of reflected EM pulses during a first period of time. In one or more embodiments, the pulse attributes engine 212 may be configured to determine a first amplitude of the first set of reflected EM pulses.
The modulator operation engine 214 may be configured to operate the modulator 110 to append a modulated signal to the set of emitted EM pulses emitted by the transmitter 102. In one or more embodiments, the modulator operation engine 212 may be configured to intermittently operate the modulator 110 to append the modulated signal to the set of emitted EM pulses. In one or more embodiments, the modulator operation engine 212 may be configured to selectively operate the modulator 110 to append the modulated signal to the set of emitted EM pulses during at least first and second periods of time, where the second period of time succeeds the first period of time. In some other embodiments, the modulator operation engine 212 may be configured to operate the modulator 110 to continuously append the modulated signal to the set of emitted EM pulses.
The pulse attributes engine 212 may be configured to determine one or more second pulse attributes related to a first set of reflected EM pulses during the second period of time. In one or more embodiments, the pulse attributes engine 212 may be configured to determine a second amplitude of the second set of reflected EM pulses.
The object location determination engine 216 may be configured to determine, based on the first and second pulse attributes, a change in position of the object 190 within the FOV 150 of the radar system 100 during a period between the first and second periods of time. In one or more embodiments, the object location determination engine 216 may be configured to determine based on the first and second amplitudes.
In one or more embodiments, the object location determination engine 216 may be configured to determine that the location of the object 190 during the first and second periods of time is substantially similar if the first and second amplitudes are substantially similar. In one or more embodiments, the object location determination engine 216 may be configured to determine that the location of the object 190 during the first and second periods of time is different if the first and second amplitudes are different.
In one or more embodiments, the modulator operation engine 214 may be configured to operate the modulator 110 to append the modulated signal to the set of emitted EM pulses during any one period of time, such that the modulated signal during any one period of time includes at least first and second frequencies different from each other.
In one or more embodiments, the pulse attributes engine 212 may be configured to determine one or more third pulse attributes related to the set of emitted EM pulses appended with the modulated signal having at least first and second frequencies. In one or more embodiments, the pulse attributes engine 212 may be configured to determine a third amplitude of set of emitted EM pulses appended with the modulated signal having at least first and second frequencies.
In one or more embodiments, the object location determination engine 216 may be configured to determine a distance of the object 190 from the receiver 104 of the radar system 100 based on the third amplitude.
Referring to
In one or more embodiments, the method 300 includes operating intermittently, by the computing device 200, the modulator 110 to append the modulated signal to the set of emitted EM pulses.
In one or more embodiments, the method 300 includes operating, by the computing device 200, the modulator 110 to continuously append the modulated signal to the set of emitted EM pulses.
In one or more embodiments, the method 300 further includes determining, by the computing device 200, the first amplitude of the first set of reflected EM pulses. The method 300 further includes determining, by the computing device 200, the second amplitude of the second set of reflected EM pulses. The method 300 further includes determining, by the computing device 200, the change in position of the object 190 based on the first and second amplitudes.
In one or more embodiments, the method 300 further includes operating, by the computing device 200, the modulator 110 to append the modulated signal to the set of emitted EM pulses during any one period of time, such that the modulated signal during the any one period of time includes at least first and second frequencies different from each other.
While the invention has been described with reference to exemplary embodiments, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention as defined by the appended claims. Modifications may be made to adopt a particular situation or material to the teachings of the invention without departing from the scope thereof. Therefore, it is intended that the invention not be limited to the particular embodiment disclosed, but that the invention includes all embodiments falling within the scope of the invention as defined by the appended claims.
In interpreting the specification, all terms should be interpreted in the broadest possible manner consistent with the context. In particular, the terms “comprises” and “comprising” should be interpreted as referring to elements, components, or steps in a non-exclusive manner, indicating that the referenced elements, components, or steps may be present, or utilized, or combined with other elements, components, or steps that are not expressly referenced. Where the specification claims refer to at least one of something selected from the group consisting of A, B, C . . . and N, the text should be interpreted as requiring only one element from the group, not A plus N, or B plus N, etc.
This patent application claims the benefit of U.S. Provisional Patent Application No. 63/583,366, filed on Sep. 18, 2023, which is incorporated by reference herein in its entirety.
| Number | Date | Country | |
|---|---|---|---|
| 63583366 | Sep 2023 | US |
