Conventional pulsed laser remote sensors perform over short distances on the order of 1 km or less. Further, they typically require high power and implement incoherent direct detection methods. In contrast, conventional coherent pulsed laser sensors interfere a scattered pulse reflected from a target with a portion of the emitted pulse which was transmitted by the laser at an earlier time. A laser having extremely narrow frequency linewidths and a coherence length of at least twice as long as the operating range of the sensor must be used to ensure interference of the scattered pulse and the emitted pulse.
In order to use temporally short pulses for coherent detection, the center frequency of the laser must be stabilized to increase its coherence length. In practice, this is complex and difficult since free running ultrafast laser systems typically have a coherence length of a single pulse duration. Thus, conventional coherent pulsed laser sensors must use a delay line equal to the round trip time-of-flight because it is necessary to interfere the scattered pulse with the same emitted pulse which produced the scattered pulse.
As a result, a low power coherent pulsed laser remote sensor having a long coherence time is desired in order to sense targets at long ranges. Further, it is desired that the laser sensor utilize amplitude and phase information contained in radiation pulses scattered by the targets to determine unique target signatures.
According to various embodiments, an ultra-stable short pulse remote sensor having extended temporal coherence for long range environmental sensing, surveillance, and reconnaissance is disclosed. In particular, the sensor determines unique target signatures after an ultrashort pulse has interacted with a target at range by measuring the spectral amplitude and phase of the scattered pulse. As a result, the ultra-stable short pulse remote sensor improves over conventional optical remote sensors by achieving coherent detection of targets with reduced power and at long range, e.g., megameter ranges. Further, the ultra-stable short pulse sensor can be implemented in a small and lightweight system using commercially available technology.
In an embodiment, a receiver is configured to detect ultrashort multispectral pulses of radiation scattered by a target, the receiver comprising a detector configured to detect scattered radiation pulses produced by scattering of emitted radiation pulses by the target; an interferometer configured to interfere the scattered pulses with a reference pulse, wherein the emitted pulses and the reference pulse are different radiation pulses in a series of pulses; and a processor configured to determine an intensity and a phase of the scattered pulses based on the interference of the scattered pulses with the reference pulse.
In a further embodiment, a method of detecting ultrashort multispectral pulses of radiation scattered by a target includes generating a series of coherent radiation pulses; selecting reference radiation pulses from the series of pulses; emitting radiation pulses from the series of pulses, wherein the reference pulses and the emitted pulses are different pulses; receiving scattered radiation pulses produced by scattering of the emitted pulses by the target; interfering the scattered pulses with the reference pulses; and determining an intensity and a phase of the scattered pulses based on the interference.
In a further embodiment, a system is configured to emit and receive ultrashort multispectral pulses of radiation, the system comprising a source configured to generate a series of radiation pulses including reference radiation pulses and emitted radiation pulses produced by scattering of the emitted radiation pulses by a target; a receiver configured to receive scattered radiation pulses produced by scattering of the emitted radiation pulses by a target; an interferometer configured to interfere the scattered pulses with reference pulses; and a processor configured to determine an intensity and a phase of the scattered pulses based on an output of the interferometer.
These and other features and advantages of the novel and non-obvious system and method will be apparent from this disclosure. It is to be understood that the summary, drawing, and detailed description are not restrictive of the scope of the inventive concept described herein.
In an embodiment, the pulses emitted from source 105 are split into a beam of high-energy pulses 115 and a beam of low-energy reference pulses 120. High-energy pulses 115 are launched toward target 125 and interact with target 125. Scattered radiation pulses 130 are reflected back to receiver 110 due to scattering of high-energy pulses 115 by target 125.
Low-energy reference pulses 120 are coupled directly from source 105 to receiver 110. Receiver 110 coherently combines low-energy pulses 120 and scattered pulses 130 to produce a signal for output or further processing. In particular, the optical information contained in scattered pulses 130 may be measured by determining the differences between scattered pulses 130 and low-energy reference pulses 120. Such analysis of scattered pulses 130 permits, e.g., discovery, detection, recognition, and/or verification of target 125. The range of transceiver 100, however, may be limited due to instability of reference pulses 120 with respect to time, and the greater time-of-flight required for pulses 115 and 130 to reach more distant targets 125.
understanding. In particular, scattered pulses 130 comprises pulse n0 205 which has been time delayed relative to reference pulses 120. The time delay results due to the time-of-flight required for pulses 115 and 130 to reflect from target 125. Pulse n0 205 is caused to interfere with pulse n0+n 210, which may be sampled directly from laser source 105 and provided by reference beam 120. In an embodiment, n is a large number of pulses emitted from source 105 during the time delay of pulse n0 205, e.g., tens, hundreds, thousands, or millions of pulses.
In one or more embodiments, a conventional delay line is not required. Conventional delay lines were necessary in previous devices due to the short coherence time of conventional laser sources which caused radiation pulses to lose coherency with subsequent pulses emitted after the coherence time. Therefore, without a conventional delay line, the coherency between a scattered pulse and a subsequent (i.e., reference) pulse would be lost by the time the scattered pulse returned from the target. As a result, conventional delay lines were provided to enable both scattered pulses 130 and the reference pulse 120 from the same source pulse 105 to be interfered. Accordingly, it was necessary to match the delay of the conventional delay line to the time-of-flight for a pulse to reach the target and to return from the target. In contrast, according to an embodiment, scattered pulse n0 205 can be interfered, e.g., with subsequent reference pulse n0+n 210, since reference pulses 120 remain coherent for an extended period of time.
In contrast, if pulse n0 205 and pulse n0+n 210 are not coherent, e.g., as in a free-running oscillator, no fringe pattern is observed, as shown by interferogram 305. Furthermore, it is not possible to detect and compensate for instantaneous intensity fluctuations in source 105. Therefore, intensity I(t) and phase φ(t) information cannot be determined. The length of time that pulse n0 205 can be coherently maintained with respect to pulse n0+n 210 limits the range to which transceiver 100 can detect target 125. Typically, conventional ultrafast lasers which operate with high repetition rates in excess of tens of MHz have short temporal coherence.
However, it is possible to increase the range of transceiver 100 by increasing the temporal coherence of source 105 so that pulse n0 205 remains coherent with pulse n0+n 210 over multiple pulses. In an embodiment, source 105 may have long term temporal stability in excess of 100 seconds. Further, such long term temporal stability enables interferogram 310 to use a multi-pulse exposure to improve the signal-to-noise ratio. For example, a one second exposure (i.e., only 1% of temporal coherence of source 105) allows interferogram 310 to be constructed from over a million pulses.
Ultra-wideband (UWB) source 910 converts the pulses produced by laser 905 to a supercontinuum of pulses having broad multispectral bandwidth, e.g. up to 500 THz. The pulses are characterized by non-linear (NL) detector 915 either before or after being provided to UWB source 910. An exemplary reference pulse 120 is shown having an intensity and phase which is representative of each of the other pulses in the pulse train.
Pulse shaping encoder (PS-E) 920 shapes the pulses for performance, e.g. in a military environment, and may have adaptive capabilities. In various embodiments, PS-E 920 can be configured as a liquid crystal spatial light modulator to adjust amplitude and phase of the individual spectral components. The pulses reflect from target 125 and pulse shaping decoder (PS-D) 925 recovers scattered pulses 130 from the signal received from target 125. The intensity and phase of an exemplary scattered pulses 130 are shown. Receiver 110 interferes reference pulse 120 with scattered pulses 130 in order to recover the signature of target 125.
In an embodiment, the repetition rate of laser 905 may be fixed relative to an ultra-stable RF source. A fixed laser repetition rate results from stabilizing the cavity length. The cavity length may be stabilized via a feedback process using phase-locked loop (PLL) 1005. PLL 1005 detects a small portion of the output of laser 905 by fast photodiode 1010 (rise time ˜1 ns). PLL 1005 compares the cavity repetition frequency with that of the RF source. An error signal is generated which adjusts piezo-electric transducer 1015 (PZT) on the end mirror of the cavity.
Having fixed the repetition rate, the carrier-envelop offset (CEO) may be stabilized. CEO describes the actual phase of the carrier wavelength inside the pulse envelope. For most pulsed laser applications, the group velocity (how the pulse envelope propagates) and the phase velocity (how the phase of the spectral components propagate) are different. This difference results in a “slip” in the carrier phase within the pulse envelope and limits the temporal coherence of laser 905. In an embodiment, locking the CEO permits measurement of scattered beam 130 using pulse n0 205 and pulse n0+n 210.
CEO may be stabilized using, e.g., f-to-2f interferometry, which requires laser 905 to have at least an octave of spectral width. In particular, PCF 1020 samples a fraction of the output of laser 905, which generates a supercontinuum spectrum. Next, a portion of the supercontinuum may be frequency doubled and heterodyned with the remaining supercontinuum. By selecting only wavelengths which are present in both spectra via a bandpass filter, a heterodyne signal is created which describes the CEO. This signal may be stabilized against a second RF source or an atomic standard, such as a Cs clock, in a similar matter as with PLL 1005. The generated error signal is, in turn, is provided as feedback to the current control on laser 905. By changing the current to laser 905, the CEO can be varied. Accordingly, source 105 has long-term stability in excess of 100 seconds, which exceeds the stability require for the receiver.
Scattered pulses 130 and reference pulse 120 collinearly propagate toward SI device 1305. The spectrum of the resulting interference pattern between scattered pulses 130 and reference pulse 120 is measured using a spectrometer. The signal from the spectrometer, called an interferogram, comprises a fringe pattern which varies as a function of wavelength. Since the interference process requires temporal overlap of both pulse 120 and 130, delay 1315 is provided to ensure that pulses 120 and 130 arrive simultaneously at SI device 1305. In an embodiment, two different pulses 120 and 130 separated by a time delay can be caused to interfere, thus enabling the detection of distant target 125. Delay 1315 is different than conventional delay lines selected based upon the target range, as discussed above. In particular, delay 1315 is selected to align scattered pulses 130 with a subsequent reference pulse 120, and is not based on time-of-flight of a pulse or target distance. In an embodiment, delay 1315 may provide a delay less than or equal to the period of train of pulses.
To acquire the optical information of scattered pulses 130, laser source 105 can be initially characterized. Standard FROG device 1310 performs the initial characterization of source 105 using reference pulses 120, and provides the amplitude and phase information specific to laser source 105. Once the optical information of source 105 is known, receiver 110 can decode the fringe pattern in the interferogram in order to retrieve the optical information of scattered pulses 130. It is not necessary, however, to perform the initial characterization on each pulse exiting laser 105 since the retrieved optical information describing laser source 105 is valid for extended time periods due to the long term stability and coherence time of source 105. Accordingly, the optical information in scattered beam 130 can be retrieved. Further, by reducing pulse energy requirements, source 105 can be simply an oscillator or an oscillator with a small amplification stage. As a result, source 105 does not require the additional complexity of high power amplification techniques, e.g., a chirp pulsed amplifier.
Processor and memory 1320 may determine a target signature based on the intensity and phase of scattered pulses 130. Further, processor and memory 1320 can be configured to compare the target signature to a database of target signatures, thus enabling target 125 to be classified and/or identified.
While particular embodiments of this disclosure have been described, it is understood that modifications will be apparent to those skilled in the art without departing from the spirit of the inventive concept. The scope of the inventive concept is not limited to the specific embodiments described herein. Other embodiments, uses, and advantages will be apparent to those skilled in art from the specification and the practice of the claimed invention.
The U.S. Government may have certain rights in this application as provided for in Cooperative Research and Development Agreement (CRADA) no. 99-RMSC-MULT-1547 executed Jul. 31, 2003.