The operation of a coherent Doppler lidar, developed by NASA for missions to planetary bodies, is analyzed and its projected performance is described. The lidar transmits three laser beams at different but fixed directions and measures line-of-sight range and velocity along each beam. The three line-of-sight measurements are then combined in order to determine the three components of the vehicle velocity vector and its altitude relative to the ground. Operating from over five kilometers altitude, the NDL provides velocity and range data with a few cm/sec and a few meters precision, respectively, depending on the vehicle dynamics. This paper explains the sources of measurements error and analyzes the impacts of vehicle dynamics on the lidar performance.
This paper describes a coherent Doppler lidar developed by NASA to address a need for a high-performance, compact, and cost-effective velocity and altitude sensor onboard its landing vehicles. Future robotic and manned missions to solar system bodies require precise ground-relative velocity vector and altitude data to execute complex descent maneuvers and soft landing at a pre-designated site. This lidar sensor, referred to as Navigation Doppler Lidar (NDL), transmits three laser beams at different pointing angles toward the ground and measures range and velocity along each beam using a frequency modulated continuous wave (FMCW) technique. The three line-of-sight measurements are then combined in order to determine the three components of the vehicle velocity vector and its altitude relative to the ground with about 2 cm/sec and 2 meters precision, respectively, dominated by the vehicle motion. The NDL can also benefit terrestrial aerial vehicles that cannot rely on GPS for position and velocity data. The NDL offers a viable option for enabling aircraft operation in areas where the GPS signal can be blocked or jammed by intentional or unintentional interference. A modified version of the NDL incorporating a beam steering device can produce 3-dimensional range and Doppler images that are critical for safe andefficient operation of autonomous ground vehicles. This paper describes the design of the NDL and its capabilities as demonstrated through extensive ground tests and flight tests onboard helicopters and autonomous rocket-powered vehicles. Then, the utilization of the NDL technologies for terrestrial vehicles will be discussed.
Future NASA exploratory missions to the Moon and Mars will require safe soft-landings at the designated sites with a high degree of precision. These sites may include areas of high scientific value with relatively rough terrain with little or no solar illumination and possibly areas near pre-deployed assets. The ability of lidar technology to provide three-dimensional elevation maps of the terrain, high precision distance to the ground, and approach velocity can enable safe landing of large robotic and manned vehicles with a high degree of precision. Currently, NASA-LaRC is developing novel lidar sensors aimed at meeting NASA’s objectives for future planetary landing missions under the Autonomous Landing and Hazard Avoidance (ALHAT) project. These lidar sensors are 3-Dimensional Imaging Flash Lidar, Doppler Lidar, and Laser Altimeter. The Flash Lidar is capable of generating elevation maps of the terrain identifying hazardous features such as rocks, craters, and steep slopes. The elevation maps collected during the approach phase between 1000 m to 500 m above the ground can be used to determine the most suitable safe landing site. The Doppler Lidar provides highly accurate ground velocity and distance data allowing for precision navigation to the selected landing site. Prior to the approach phase at altitudes of over 15 km, the Laser Altimeter can provide sufficient data for updating the vehicle position and attitude data from the Inertial Measurement Unit. At these higher altitudes, either the Laser Altimeter or the Flash Lidar can be used for generating a contour map of the terrain below for identifying known surface features such as craters for further reducing the vehicle relative position error.
Future NASA exploratory missions to the Moon and Mars will require safe soft-landings at the designated sites with a high degree of precision. These sites may include areas of high scientific value with relatively rough terrain with little or no solar illumination and possibly areas near pre-deployed assets. The ability of lidar technology to provide three-dimensional elevation maps of the terrain, high precision distance to the ground, and approach velocity can enable safe landing of large robotic and manned vehicles with a high degree of precision. Currently, NASA-LaRC is developing novel lidar sensors aimed at meeting NASA’s objectives for future planetary landing missions under the Autonomous Landing and Hazard Avoidance (ALHAT) project [1]. These lidar sensors are 3-Dimensional Imaging Flash Lidar, Doppler Lidar, and Laser Altimeter. The Flash Lidar is capable of generating elevation maps of the terrain identifying hazardous features such as rocks, craters, and steep slopes. The elevation maps collected during the approach phase between 1000 m to 500 m above the ground can be used to determine the most suitable safe landing site. The Doppler Lidar provides highly accurate ground velocity and distance data allowing for precision navigation to the selected landing site. Prior to the approach phase at altitudes of over 15 km, the Laser Altimeter can provide sufficient data for updating the vehicle position and attitude data from the Inertial Measurement Unit. At these higher altitudes, either the Laser Altimeter or the Flash Lidar can be used for generating a contour map of the terrain below for identifying known surface features such as craters for further reducing the vehicle relative position error.
A coherent Doppler lidar has been developed to address NASA’s need for a high-performance, compact, and cost-effective velocity and altitude sensor onboard its landing vehicles. Future robotic and manned missions to solar system bodies require precise ground-relative velocity vector and altitude data to execute complex descent maneuvers and safe, soft landing at a pre-designated site. This lidar sensor, referred to as a Navigation Doppler Lidar (NDL), meets the required performance of the landing missions while complying with vehicle size, mass, and power constraints. Operating from up to four kilometers altitude, the NDL obtains velocity and range precision measurements reaching 2 cm/sec and 2 meters, respectively, dominated by the vehicle motion. Terrestrial aerial vehicles will also benefit from NDL data products as enhancement or replacement to GPS systems when GPS is unavailable or redundancy is needed. The NDL offers a viable option to aircraft navigation in areas where the GPS signal can be blocked or jammed by intentional or unintentional interference. The NDL transmits three laser beams at different pointing angles toward the ground to measure range and velocity along each beam using a frequency modulated continuous wave (FMCW) technique. The three line-of-sight measurements are then combined in order to determine the three components of the vehicle velocity vector and its altitude relative to the ground. This paper describes the performance and capabilities that the NDL demonstrated through extensive ground tests, helicopter flight tests, and onboard an autonomous rocket-powered test vehicle while operating in closedloop with a guidance, navigation, and control (GN and C) system.
KEYWORDS: LIDAR, Sensors, Space operations, Doppler effect, Solar system, Mars, Imaging systems, 3D image processing, Navigation systems, Algorithm development
NASA has been pursuing flash lidar technology for autonomous, safe landing on solar system bodies and for automated rendezvous and docking. During the final stages of landing, from about 1 km to 500 m above the ground, the flash lidar can generate 3-Dimensional images of the terrain to identify hazardous features such as craters, rocks, and steep slopes. The onboard flight computer can then use the 3-D map of terrain to guide the vehicle to a safe location. As an automated rendezvous and docking sensor, the flash lidar can provide relative range, velocity, and bearing from an approaching spacecraft to another spacecraft or a space station. NASA Langley Research Center has developed and demonstrated a flash lidar sensor system capable of generating 16k pixels range images with 7 cm precision, at a 20 Hz frame rate, from a maximum slant range of 1800 m from the target area. This paper describes the lidar instrument and presents the results of recent flight tests onboard a rocket-propelled free-flyer vehicle (Morpheus) built by NASA Johnson Space Center. The flights were conducted at a simulated lunar terrain site, consisting of realistic hazard features and designated landing areas, built at NASA Kennedy Space Center specifically for this demonstration test. This paper also provides an overview of the plan for continued advancement of the flash lidar technology aimed at enhancing its performance to meet both landing and automated rendezvous and docking applications.
KEYWORDS: Sensors, LIDAR, Data modeling, Detection and tracking algorithms, Statistical modeling, Navigation systems, Algorithm development, Evolutionary algorithms, Monte Carlo methods, 3D image processing
NASA’s Autonomous Landing and Hazard Avoidance Technologies (ALHAT) project is currently developing the critical technologies to safely and precisely navigate and land crew, cargo and robotic spacecraft vehicles on and around planetary bodies. One key element of this project is a high-fidelity Flash Lidar sensor that can generate three-dimensional (3-D) images of the planetary surface. These images are processed with hazard detection and avoidance and hazard relative navigation algorithms, and then are subsequently used by the Guidance, Navigation and Control subsystem to generate an optimal navigation solution. A complex, high-fidelity model of the Flash Lidar was developed in order to evaluate the performance of the sensor and its interaction with the interfacing ALHAT components on vehicles with different configurations and under different flight trajectories. The model contains a parameterized, general approach to Flash Lidar detection and reflects physical attributes such as range and electronic noise sources, and laser pulse temporal and spatial profiles. It also provides the realistic interaction of the laser pulse with terrain features that include varying albedo, boulders, craters slopes and shadows. This paper gives a description of the Flash Lidar model and presents results from the Lidar operating under different scenarios.
A high precision laser altimeter was developed under the Autonomous Landing and Hazard Avoidance (ALHAT) project at NASA Langley Research Center. The laser altimeter provides slant-path range measurements from operational ranges exceeding 30 km that will be used to support surface-relative state estimation and navigation during planetary descent and precision landing. The altimeter uses an advanced time-of-arrival receiver, which produces multiple signal-return range measurements from tens of kilometers with 5 cm precision. The transmitter is eye-safe, simplifying operations and testing on earth. The prototype is fully autonomous, and able to withstand the thermal and mechanical stresses experienced during test flights conducted aboard helicopters, fixed-wing aircraft, and Morpheus, a terrestrial rocket-powered vehicle developed by NASA Johnson Space Center. This paper provides an overview of the sensor and presents results obtained during recent field experiments including a helicopter flight test conducted in December 2012 and Morpheus flight tests conducted during March of 2014.
Landing mission concepts that are being developed for exploration of solar system bodies are increasingly ambitious in
their implementations and objectives. Most of these missions require accurate position and velocity data during their
descent phase in order to ensure safe, soft landing at the pre-designated sites. Data from the vehicle’s Inertial
Measurement Unit will not be sufficient due to significant drift error after extended travel time in space. Therefore, an
onboard sensor is required to provide the necessary data for landing in the GPS-deprived environment of space. For this
reason, NASA Langley Research Center has been developing an advanced Doppler lidar sensor capable of providing
accurate and reliable data suitable for operation in the highly constrained environment of space. The Doppler lidar
transmits three laser beams in different directions toward the ground. The signal from each beam provides the platform
velocity and range to the ground along the laser line-of-sight (LOS). The six LOS measurements are then combined in
order to determine the three components of the vehicle velocity vector, and to accurately measure altitude and attitude
angles relative to the local ground. These measurements are used by an autonomous Guidance, Navigation, and Control
system to accurately navigate the vehicle from a few kilometers above the ground to the designated location and to
execute a gentle touchdown. A prototype version of our lidar sensor has been completed for a closed-loop demonstration
onboard a rocket-powered terrestrial free-flyer vehicle.
The ability of lidar technology to provide three-dimensional elevation maps of the terrain, high precision distance to the
ground, and approach velocity can enable safe landing of robotic and manned vehicles with a high degree of precision.
Currently, NASAis developing novel lidar sensors aimed at the needs of future planetary landing missions.These lidar
sensors are a 3-Dimensional Imaging Flash Lidar, a Doppler Lidar, and a Laser Altimeter. The Flash Lidar is capable of generating elevation maps of theterrain toindicate hazardous features such as rocks, craters, and steep slopes. The
elevation maps, which arecollected during the approach phase of a landing vehicle from about 1 km above the ground,
can be used to determine the most suitable safe landing site. The Doppler Lidar provides highly accurate ground relative
velocity and distance data thusenablingprecision navigation to the landing site. Our Doppler lidar utilizes three laser
beams that are pointed indifferent directions to measure line-of-sight velocities and ranges to the ground from altitudes
of over 2 km.Starting at altitudes of about 20km and throughout the landing trajectory,the Laser Altimeter can provide
very accurate ground relative altitude measurements that are used to improve the vehicle position knowledge obtained from the vehicle'snavigation system. Betweenaltitudesof approximately 15 km and 10 km, either the Laser Altimeter
or the Flash Lidar can be used to generate contour maps of the terrain, identifying known surface features such as craters to perform Terrain relative Navigation thus further reducing the vehicle's relative position error. This paper describes the
operational capabilities of each lidar sensorand provides a status of their development.
KEYWORDS: Sensors, Velocity measurements, Doppler effect, LIDAR, Navigation systems, Signal processing, Receivers, Global Positioning System, Signal to noise ratio, Control systems
An all fiber Navigation Doppler Lidar (NDL) system is under development at NASA Langley Research Center
(LaRC) for precision descent and landing applications on planetary bodies. The sensor produces high-resolution
line of sight range, altitude above ground, ground relative attitude, and high precision velocity vector measurements.
Previous helicopter flight test results demonstrated the NDL measurement concepts, including measurement
precision, accuracies, and operational range. This paper discusses the results obtained from a recent campaign to
test the improved sensor hardware, and various signal processing algorithms applicable to real-time processing. The
NDL was mounted in an instrumentation pod aboard an Erickson Air-Crane helicopter and flown over various
terrains. The sensor was one of several sensors tested in this field test by NASA's Autonomous Landing and Hazard
Avoidance Technology (ALHAT) project.
A novel method for enhancement of the spatial resolution of 3-diminsional Flash Lidar images is being proposed for
generation of elevation maps of terrain from a moving platform. NASA recognizes the Flash LIDAR technology as
an important tool for enabling safe and precision landing in future unmanned and crewed lunar and planetary
missions. The ability of the Flash LIDAR to generate 3-dimensional maps of the landing site area during the final
stages of the descent phase for detection of hazardous terrain features such as craters, rocks, and steep slopes is
under study in the frame of the Autonomous Landing and Hazard Avoidance (ALHAT) project. Since single frames
of existing FLASH LIDAR systems are not sufficient to build a map of entire landing site with acceptable spatial
resolution and precision, a super-resolution approach utilizing multiple frames has been developed to overcome the
instrument's limitations. Performance of the super-resolution algorithm has been analyzed through a series of
simulation runs obtained from a high fidelity Flash LIDAR model and a high resolution synthetic lunar elevation
map. For each simulation run, a sequence of FLASH LIDAR frames are recorded and processed as the spacecraft
descends toward the landing site. Simulations runs having different trajectory profiles and varying LIDAR look
angles of the terrain are also analyzed. The results show that adequate levels of accuracy and precision are achieved
for detecting hazardous terrain features and identifying safe areas of the landing site.
KEYWORDS: LIDAR, Space operations, Sensors, Detection and tracking algorithms, Data modeling, Super resolution, Image processing, 3D image processing, Image resolution, Signal processing
In this paper a new image processing technique for flash LIDAR data is presented as a potential tool to enable
safe and precise spacecraft landings in future robotic or crewed lunar and planetary missions. Flash LIDARs
can generate, in real-time, range data that can be interpreted as a 3-dimensional (3-D) image and transformed
into a corresponding digital elevation map (DEM). The NASA Autonomous Landing and Hazard Avoidance
(ALHAT) project is capitalizing on this new technology by developing, testing and analyzing flash LIDARs
to detect hazardous terrain features such as craters, rocks, and slopes during the descent phase of spacecraft
landings. Using a flash LIDAR for this application looks very promising, however through theoretical and
simulation analysis the ALHAT team has determined that a single frame, or mosaic, of flash LIDAR data may
not be sufficient to build a landing site DEM with acceptable spatial resolution, precision, size, or for a mosaic,
in time, to meet current system requirements. One way to overcome this potential limitation is by enhancing
the flash LIDAR output images. We propose a new super-resolution algorithm applicable to flash LIDAR range
data that will create a DEM with sufficient accuracy, precision and size to meet current ALHAT requirements.
The performance of our super-resolution algorithm is analyzed by processing data generated during a series of
simulation runs by a high fidelity model of a flash LIDAR imaging a high resolution synthetic lunar elevation
map. The flash LIDAR model is attached to a simulated spacecraft by a gimbal that points the LIDAR to a
target landing site. For each simulation run, a sequence of flash LIDAR frames is recorded and processed as
the spacecraft descends toward the landing site. Each run has a different trajectory profile with varying LIDAR
look angles of the terrain. We process the output LIDAR frames using our SR algorithm and the results show
that the achieved level of accuracy and precision of the SR generated landing site DEM is more than adequate
for detecting hazardous terrain features and identifying safe areas.
NASA considers Flash Lidar a critical technology for enabling autonomous safe landing of future large robotic and
crewed vehicles on the surface of the Moon and Mars. Flash Lidar can generate 3-Dimensional images of the terrain to
identify hazardous features such as craters, rocks, and steep slopes during the final stages of descent and landing. The
onboard flight comptuer can use the 3-D map of terain to guide the vehicle to a safe site.
The capabilities of Flash Lidar technology were evaluated through a series of static tests using a calibrated target and
through dynamic tests aboard a helicopter and a fixed wing airctarft. The aircraft flight tests were perfomed over Moonlike
terrain in the California and Nevada deserts. This paper briefly describes the Flash Lidar static and aircraft flight test
results. These test results are analyzed against the landing application requirements to identify the areas of technology
improvement. The ongoing technology advancement activities are then explained and their goals are described.
Data from the first Flight Test of the NASA Langley Flash Lidar system have been processed. Results of the
analyses are presented and discussed. A digital elevation map of the test site is derived from the data, and is
compared with the actual topography. The set of algorithms employed, starting from the initial data sorting, and
continuing through to the final digital map classification is described. The accuracy, precision, and the spatial and
angular resolution of the method are discussed.
KEYWORDS: LIDAR, Global Positioning System, Doppler effect, Sensors, Velocity measurements, Signal to noise ratio, Modulation, Receivers, Signal processing
A navigation Doppler Lidar (DL) was developed at NASA Langley Research Center (LaRC) for high precision velocity
measurements from a lunar or planetary landing vehicle in support of the Autonomous Landing and Hazard Avoidance
Technology (ALHAT) project. A unique feature of this DL is that it has the capability to provide a precision velocity
vector which can be easily separated into horizontal and vertical velocity components and high accuracy line of sight
(LOS) range measurements. This dual mode of operation can provide useful information, such as vehicle orientation
relative to the direction of travel, and vehicle attitude relative to the sensor footprint on the ground. System performance
was evaluated in a series of helicopter flight tests over the California desert. This paper provides a description of the DL
system and presents results obtained from these flight tests.
A high repetition rate, wavelength agile heterodyne detection lidar system is being developed at Coherent Applications,
Inc. (CAI). The motivation behind this endeavor is the potential ultra-high sensitivity of heterodyne detection for
measuring the low intensity signals of long-range measurements of aerosols. Since speckle noise limits the overall
signal-to-noise for each pulse to a maximum of unity, important considerations in heterodyne detection system design
are the tradeoffs using lower energy pulses at high pulse repetition frequency (prf) compared with high-energy pulses at
low prf. Differential scattering/differential absorption lidar (DISC/DIAL) measurements require precise determination
of ratios of the signal levels at two or more wavelengths, and measurements need to be completed within a brief period,
so that conditions remain constant. The additional requirement to average a large number of pulses to overcome speckle
noise dictates that a high pulse repetition rate is needed. Detection sensitivity is further increased by reducing the
receiver bandwidth, and this requires that the optical frequencies of the transmitter and the local oscillator lasers must be
maintained with a stable and fixed offset relative to each other at the heterodyne intermediate frequency. This paper
provides a general description of the aerosol lidar system that integrates high-speed laser stabilization and intermediate
frequency locking of two wavelength agile lasers for heterodyne detection lidar.
Future robotic and crewed lunar missions will require safe and precision soft-landing at scientifically interesting sites
near hazardous terrain features such as craters and rocks or near pre-deployed assets. Presently, NASA is studying the
ability of various 3-dimensional imaging sensors particularly lidar/ladar techniques in meeting its lunar landing needs.
For this reason, a Sensor Test Range facility has been developed at NASA Langley Research Center for calibration and
characterization of potential 3-D imaging sensors. This paper describes the Sensor Test Range facility and its application
in characterizing a 3-D imaging ladar. The results of the ladar measurement are reported and compared with simulated
image frames generated by a ladar model that was also developed as part of this effort. In addition to allowing for
characterization and evaluation of different ladar systems, the ladar measurements at the Sensor Test Range will support
further advancement of ladar systems and development of more efficient and accurate image reconstruction algorithms.
KEYWORDS: Heterodyning, Receivers, Signal to noise ratio, Absorption, Signal detection, Chemical detection, Oscillators, Transmitters, Bragg cells, Speckle
A high repetition rate, wavelength agile CO2 laser has been developed at the Air Force Research Laboratory for use as a local oscillator in a heterodyne detection receiver. Rapid wavelength selection is required for measurements of airborne chemical vapors using the differential absorption lidar (DIAL) technique. Acousto-optic modulators are used in the local oscillator to tune between different wavelengths at high speeds (greater than 100 Hz) without the need for moving mechanical parts. Other advantages obtained by the use of acousto-optic modulators are laser output power control per wavelength and rugged packaging for field applications. A series of experiments to simultaneously characterize the radiometric and chemical detection sensitivities of heterodyne and direct detection DIAL systems is being performed at Kirtland AFB, NM, and will be described. The wavelength agile local oscillator (WALO) has been incorporated into a heterodyne receiver, with the Laser Airborne Remote Sensing (LARS) system providing the laser transmitter and direct detection receiver. The experiment series is studying radiometric issues, spread spectrum operation, the effects of target-induced speckle, and the influence of atmospheric turbulence for both detection mechanisms. Measurements are being performed over a horizontal path at standoff ranges of 4 to 15 km, using both natural and man-made targets. Comparisons of the heterodyne and direct detection radiometric and chemometric results will be presented, and contrasted with predictions from simulations and models. The results will also be discussed in terms of the implications for fielding operational DIAL systems.
A high repetition rate, wavelength agile CO2 laser has been developed at the Air Force Research Laboratory for use as a local oscillator in a heterodyne detection receiver. Rapid wavelength selection is required for measurements of airborne chemical vapors using the differential absorption lidar (DIAL) technique. Acousto-optic modulators are used in the local oscillator to tune between different wavelengths at high speeds (greater than 100 Hz) without the need for moving mechanical parts. Other advantages obtained by the use of acousto-optic modulators are laser output power control per wavelength and rugged packaging for field applications.
A series of experiments to simultaneously characterize the radiometric and chemical detection sensitivities of heterodyne and direct detection DIAL systems is being performed at Kirtland AFB, NM, and will be described. The wvelength agile local oscillator (WALO) has been incorporated into a heterodyne receiver, with the Laser Airborne Remote Sensing (LARS) system providing the laser transmitter and direct detection receiver. The experiment series is studying radiometric issues, spread spectrum operation, the effects of target-induced speckle, and the influence of atmospheric turbulence for both detection mechanisms. Direct comparisons of the heterodyne and direct detection results will be presented, and the results will also be discussed in terms of the implications for fielding operational DIAL systems.
A high repetition rate, wavelength agile CO2 laser has been developed at the Air Force Research Laboratory for use as a local oscillator in a heterodyne detection receiver. Fats wavelength selection is required for measurements of airborne chemical vapors using the differential absorption lidar (DIAL) technique. Acousto-optic modulator are used to tune between different wavelengths at high speeds without the need for moving mechanical parts. Other advantages obtained by the use of acousto-optic modulators are laser output power control per wavelength and rugged packaging for field applications. The local oscillator design is described, and the results from laboratory DIAL measurements are presented. The coherent remote optical sensor system is an internal research project being conducted by the Air Force Research Laboratory Directed Energy Directorate, Active Remote Sensing Branch. The objective of the project is to develop a new long-range standoff spectral sensor that takes advantage of the enhanced performance capabilities coherent detection can provide. Emphasis of the development is on a low cost, compact, and rugged active sensor exclusively designed for heterodyne detection using the differential absorption lidar technique. State of the art technologies in waveguide laser construction and acousto- optics make feasible the next generation of lasers capable of supporting coherent lidar system requirements. Issues addressed as part of the development include optoelectronic engineering of a low cost rugged system, and fast data throughput for real time chemical concentration measurements. All hardware used in this sensor are off-the- shelf items, so only minor hardware modifications were required for the system as it stands. This paper describes a high-speed heterodyne detection CO2 DIAL system that employs a wavelength agile, acousto-optically tuned local oscillator in the receiver. Sample experimental data collected in a controlled environment are presented as well. Chemical detection using 12 wavelengths at 200 pulses per second has been demonstrated. Initial progress on experiments to make a direct, simultaneous comparison of heterodyne and direct detection DIAL systems will also be described.
Preliminary experiments toward the implementation of Doppler spectral scanning differential absorption lidar (DSS DIAL) are described. In separate tests, CO2 laser pulses were reflected from either a ground-based retroreflector (36-km round-trip distance) or a retroreflector on the GEOS-3 satellite (approximately 2000-km round-trip distance). The returns were split into a reference channel and an absorptive gas-cell channel. The light was coherently detected with heterodyne receivers and analyzed. Results from the ground-based system produced data that matched expected values in one case but its repeatability remains to be determined. We are currently investigating the satellite-based system to assess the DSS DIAL technique.
Experimental chemical detection and radiometric results are presented from recent coherent differential absorption lidar (DIAL) ground tests conducted over four kilometer horizontal path at the Air Force Research Laboratory. Heterodyne data was collected simultaneously with the Laser Airborne Remote Sensing direct detection DIAL sensor for comparison. A brief system description of the bistatic coherent DIAL system is presented. These experiments illustrate some of the technological challenges encountered in the implementation of a wavelength-agile coherent chemical detection system.
KEYWORDS: Absorption, Receivers, Heterodyning, Carbon dioxide lasers, Sensors, Chemical analysis, LIDAR, Chemical detection, Carbon dioxide, Control systems
The Air Force Research Laboratory (AFRL) Active Remote Sensing Branch has developed the Laser Airborne Remote Sensing (LARS) system for long standoff range chemical detection using the differential absorption lidar (DIAL) technique. The system is based on a high-power CO2 laser which uses either the 12C16O2 or the 13C16O2 carbon dioxide isotopes as the lasing medium, and has output energies of up to 5 J on the stronger laser transitions. The lidar system is mounted on a flight-qualified optical breadboard designed for installation in the AFRL Argus C-135E optical testbed aircraft. This paper will present chemical detection results and issues arising from ground tests of the system performed from September to December 1998. Recent advances in implementing a frequency-agile heterodyne receiver to further increase the standoff range of the DIAL system will also be presented.
The Air Force Research Laboratory (AFRL) Active Remote Sensing Branch has developed the Laser Airborne Remote Sensing (LARS) system for chemical detection using the differential absorption lidar technique. The system is based on a high-power CO2 laser which can use either the standard 12C16O2 or the 13C16O2 carbon dioxide isotopes as the lasing medium, and has output energies of up to 5 J on the stronger laser transitions. The lidar system is mounted on a flight-qualified optical breadboard designed for installation into the AFRL Argus C- 135E optical testbed aircraft. The Phase I ground tests were conducted at Kirtland AFB in 1997, prior to the LARS flight tests performed in September 1997 at Kirtland AFB and the Idaho National Engineering and Environmental Laboratory. The Phase II ground tests were conducted in 1998 to determine the optimum performance of the LARS systems, after the incorporation of modifications and improvements suggested by the flight test results. This paper will present some of the chemical detection and radiometric results obtained during the Phase II ground tests. Following the presentation of the direct detection results, a summary of current work on a heterodyne DIAL system is given.
A wavelength agile coherent LIDAR system is under development at the Air Force Research Laboratory (AFRL). Coherent lidar has the potential of longer-range sensitivity than conventional direct detection systems. AFRL is conducting risk reduction experiments to address issues involved with coherent LIDAR. Issues include speckle noise inherent to heterodyne detection, robust signal analysis algorithm development, and integration of a wavelength agile laser as the local oscillator to the receiver. The transmitter laser, developed for the LARS program, is a high energy TE CO2 laser hardened for airborne operations. Performance of the wavelength agile local oscillator laser is presented, and preliminary data from risk reduction experiments.
The Air Force Research Laboratory has developed and tested an airborne CO2 differential absorption lidar system for the remote detection of chemicals. The Laser Airborne Remote Sensing DIAL system uses topographic backscatter to provide a long-range measurement of the column-content absorption of chemical plumes in the path of the laser beam. A high-power CO2 laser, capable of operation on multiple isotopes, and a Mersenne telescope constitute the major transceiver components. In addition to the laser, telescope, and transceiver optics, several onboard diagnostic instruments were mounted on the flight bench to monitor and optimize the system performance during airborne operation. The flight bench, electronics racks, and data acquisition and experiment control stations were designed to be integrated onto the AFRL C-135E research aircraft, and to utilize the existing pointing and tracking system on the aircraft.
The Air Force Phillips Laboratory is in the process of demonstrating an advanced space surveillance capability with a heterodyne laser radar system to be used, among other applications, for range-resolved imaging of orbiting satellites. In this paper, we present our first satellite feature reconstruction from field results using reflective tomographic techniques.
The U.S. Air Force Phillips Laboratory is evaluating the feasibility of long-standoff-range remote sensing of gaseous species present in trace amounts in the atmosphere. To date, the Phillips Laboratory program has been concerned with the preliminary design and performance analysis of a commercially available CO2 laser-based DIAL system operating from mountain-top-observatory and airborne platform and more recently with long-range ground testing using a 21.8 km slant path from 3.05 km ASL to sea level as the initial steps in the design and development of an airborne system capability. Straightforward scaling of the performance of a near-term technology direct-detection LIDAR system with propagation range to a topographic target and with the average atmospheric absorption coefficient along the path has been performed. Results indicate that useful airborne operation of such a system should be possible for slant path ranges between 20 km and 50 km, depending upon atmospheric transmission at the operating wavelengths of the 13C16O2 source. This paper describes the design of the airborne system which will be deployed on the Phillips Laboratory NC-135 research aircraft for DIAL system performance tests at slant ranges of 20 km to 50 km, scheduled for the near future. Performance simulations for the airborne tests will be presented and related to performance obtained during initial ground-based tests.
A laser long range remote sensing (LRS) program is being conducted by the United States Air Force Phillips Laboratory (AF/PL). As part of this program, AF/PL is testing the feasibility of developing a long path CO2 laser-based DIAL system for remote sensing. In support of this program, the AF/PL has recently completed an experimental series using a 21 km slant- range path (3.05 km ASL transceiver height to 0.067 km ASL target height) at its Phillips Laboratory Air Force Maui Optical Station (AMOS) facility located on Maui, Hawaii. The dial system uses a 3-joule, 13C isotope laser coupled into a 0.6 m diameter telescope. The atmospheric optical characterization incorporates information from an infrared scintillometer co-aligned to the laser path, atmospheric profiles from weather balloons launched from the target site, and meteorological data from ground stations at AMOS and the target site. In this paper, we report a description of the experiment configuration, a summary of the results, a summary of the atmospheric conditions and their implications to the LRS program. The capability of such a system for long-range, low-angle, slant-path remote sensing is discussed. System performance issues relating to both coherent and incoherent detection methods, atmospheric limitations, as well as, the development of advanced models to predict performance of long range scenarios are presented.
The Air Force Phillips Laboratory is in the process of demonstrating an advanced space surveillance capability with a heterodyne laser radar system to be used, among other applications, for range-resolved imaging and orbital element set determination. It has been shown using theory and computer simulations that superior image quality is obtained by first converting the heterodyne returns into intensity projections before using tomographic techniques to reconstruct an image, as compared to using tomographic techniques on the E- field projections directly. In this paper, data from recent field experiments is used to validate this theory. In addition, the field data is used to determine the closing velocity of an orbiting satellite as a function of time.
In the field of laser radars, there has been limited work on long-wave pulse-burst waveforms with pulse widths in the nanosecond regime. This waveform has several advantages over other waveforms, e.g., excellent range resolution with small doppler ambiguities. Phillips Lab has developed a flexible ladar to provide the means of obtaining images and signatures of hard body objects under controlled laboratory conditions. The transmitter laser is also capable of frequency agility operation to support remote sensing experiments. A coherent, pulse-tone, pulse-burst CO2 TEA laser radar operating at 10.6 micrometers is described. The pulse train is obtained by actively mode locking with an intracavity germanium standing wave acousto- optic modulator. Approximately two hundred pulses per burst are transmitted at a repetition rate of 83 MHz. Injection seeding and cavity matching produces a pulse tone waveform. An overall transceiver system bandwidth of 1 GHz is employed. The device was developed as a flexible platform to support scaled risk reduction and phenomenology experiments.
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