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Full text of "NASA Technical Reports Server (NTRS) 20090024228: Development of a Compact, Pulsed, 2-Micron, Coherent-Detection, Doppler Wind Lidar Transceiver; and Plans for Flights on NASA's DC-8 and WB-57 Aircraft"

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Development of a Compact, Pulsed, 2-Micron, Coherent-Detection, Doppler 
Wind Lidar Transceiver; and Plans for Flights on NASA’s DC-8 and WB-57 

Aircraft 


Michael J. Kavaya, Upendra N. Singh, Grady J. Koch, Jirong Yu, Bo Trieu 

NASA Langley Research Center 
Mail Code 468, Hampton, Virginia 23681 USA 
michael.j .kavaya@nasa.gov 

Mulugeta Petros 

Science and Technology Corporation 
101 Research Drive, Hampton, Virginia 23666 USA 

Paul Petzar 

National Institute of Aerospace 
100 Exploration Way, Hampton, Virginia 23668 USA 


Abstract 

We present results of a recently completed effort to design, fabricate, and demonstrate a compact lidar transceiver for 
coherent-detection lidar profiling of winds. The novel high-energy, 2-micron, Ho:Tm:LuLiF laser technology 
developed at NASA Langley was employed to permit study of the laser technology currently envisioned by NASA for 
global coherent Doppler lidar measurement of winds in the future. The 250 mJ, 10 Hz compact transceiver was also 
designed for future aircraft flight. Ground-based wind profiles made with this transceiver will be presented. NASA 
Langley is currently funded to build complete Doppler lidar systems using this transceiver for the DC-8 and WB-57 
aircraft. The WB-57 flights will present a more severe environment and will require autonomous operation of the lidar 
system. The DC-8 lidar system is a likely component of future NASA hurricane research. It will include real-time data 
processing and display, as well as full data archiving. We will attempt to co-fly on both aircraft with a direct-detection 
Doppler wind lidar system being prepared by NASA Goddard Space Flight Center. 

1 Motivation 

The global measurement of horizontal wind profiles from space has been strongly endorsed by the National Oceanic 
and Atmospheric Administration (NOAA), the Integrated Program Office-National Polar-orbiting Operational 
Environmental Satellite Systems (IPO-NPOESS), the United States Air Force (USAF), and the National Aeronautics 
and Space Administration (NASA). Recently, the National Research Council (NRC) included the wind mission as one 
of fifteen missions recommended for NASA implementation in their earth science decadal survey (DS) 1 . 



After much study, NOAA, NASA, IPO, and the NRC agree that the sensor for the wind mission should be a hybrid 
Doppler wind lidar (HDWL) comprising a pulsed coherent-detection Doppler wind lidar (CDWL) at 2 microns and a 
pulsed direct-detection Doppler wind lidar (DDWL) at 0.355 microns. Within NASA this laser and lidar technology is 
being develop at Langley Research Center (LaRC) and Goddard Space Flight Center (GSFC), respectively 2 . 

2 Space-Based Wind Measurement Requirements 

NOAA and NASA scientists have worked together with academia to develop wind measurement requirements for the 
two missions endorsed by the NRC DS: the science demonstration mission, and the operational mission. NASA and 
NOAA lidar technologists participated in the process to eliminate uncertainties in the meaning of the requirements. 
These comprehensive requirements are published in a NASA report 3 . 

3 Computer Simulation of Space-Based Wind Measurement 

The linkage between the wind measurement requirements and the lidar hardware is a collection of computer simulations 
at LaRC, GSFC, and Simpson Weather Associates (SWA) 4 . In particular the SWA simulation has a sophisticated model 
of the atmosphere. It has been used to determine coherent and direct Doppler lidar parameters for the two NRC DS 
wind missions. Some of the coherent lidar parameters for the first space winds mission are 0.25 J pulse energy, 5 Hz 
pulse repetition frequency (PRF), and 0.5 m receiver diameter. 

4 Coherent Doppler Wind Lidar Technology Development at LaRC 

NASA LaRC has been developing coherent Doppler wind lidar technology continuously since the 1980s. The major 
portion of this effort has been the pulsed, 2-micron, long-pulse transmitter laser. Since 2002 this work has been 
performed under the Laser Risk Reduction Program (LRRP), a joint program at LaRC and GSFC. The LaRC 2-micron 
laser development under LRRP has been comprised of advancing pulse energy, pulse repetition frequency, beam 
quality, electrical efficiency, conductive cooling, compactness, and lifetime. Successes include partially conductively 
cooled pulse energy of 1.2 J 5 , fully conductively cooled pulse energy of 0.4 J 6 , pump laser diode array advancement, 
and demonstration of ground-based wind measurement 7 . 

5 The DAWN 2-Micron Pulsed Coherent Doppler Wind Lidar Transceiver 

The Doppler Aerosol WiNd lidar (DAWN) project at LaRC sought to place the state-of-the-art pulsed 2-micron laser 
technology into a compact, engineered package for later aircraft flights. DAWN packaged the transceiver portion of the 
Doppler lidar system using conductively cooled pump laser diode arrays and a liquid cooled laser rod (partially 
conductively cooled). The transceiver of a lidar system comprises all transmit and receive optics except for the 
telescope and scanner, (see Figure 1 below) The completed DAWN transceiver, shown in Figure 2 below, is 
approximately 15 x 29 x 67 cm, and has a mass of 34 kg. It currently produces 0.25 J pulse energy at 5 Hz PRF. It will 
soon be capable of 1 0 Hz. 

The DAWN transceiver was transported to the LaRC VALID AR (VALIDation LIDAR) and aligned with the existing 
15 cm off-axis, reflecting telescope and full hemispheric scanner. With no internal alignment needed, it measured winds 
in Hampton, Virginia to greater heights than previously seen. As part of a separate NASA project, DAWN and 
VALID AR were transported to Beltsville, Maryland for intercomparisons of wind measurements with GSFC's Doppler 
lidar and with other sensors. The DAWN transceiver did not need any re-alignment after the highway trip. It performed 
very well and could be left unattended for long periods of time. Figure 3 shows both horizontal and vertical wind 
profiles vs. altitude for an unattended 14 hour period on March 11-12, 2009. The abscissa is time and the ordinate is 



altitude from 0 to 7500 m for all 4 data panels. From top to bottom the data panels are horizontal wind speed, horizontal 
wind direction, vertical wind speed, and vertical signal power. The horizontal wind profile is measured using two 
orthogonal azimuth angles and a 45 degree elevation angle. The vertical wind profile is measured with a third zenith 
direction. The wind data are plotted with 3-minute shot integration times to obtain a profile. The 14 hours of data 
contain about 280 of these wind profiles. 

LaRC is currently busy developing lidar systems using DAWN for the DC-8 and WB-57 aircraft. Co-flights with 
GSFC's direct detection Doppler lidar are planned. 



Figure 1. Diagram showing transceiver portion of lidar system addressed by DAWN 



Figure 2. The DAWN pulsed, 2-micron, coherent Doppler wind lidar transceiver 






Altitude (m) Altitude (m) Altitude (m) 


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Figure 3. DAWN-VALIDAR horizontal and vertical wind data over 14 hours and with unattended operation 


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6 Acknowledgements 

The authors appreciate the support of Dr. Ramesh K. Kakar, George J. Komar, and Janice L. Buckner of NASA HQ. 

7 References 

1. National Research Council (NRC), “Earth Science and Applications from Space: National Imperatives for the 
Next Decade and Beyond,” The National Academies Press, Wash DC, (Jan. 2007), “Decadal Survey” 

2. M. J. Kavaya, J. Yu, G. J. Koch, F. Amzajerdian, U. N. Singh, and G. D. Emmitt, “Requirements and Technology 
Advances for Global Wind Measurement with a Coherent Lidar: A Shrinking Gap,” Proc. SPIE Vol. 6681, Lidar 
Remote Sensing for Environmental Monitoring VIII, San Diego, CA (26-30 August 2007) 

3. A. Valinia, J. Neff, C. Edwards, S. Ismail, M. J. Kavaya, U. N. Singh, M. Vaughn, et al, “Lidar Technologies 
Working Group Report,” Final Report of the NASA Earth Science Technology Office (ESTO) Laser/Lidar 
Technology Requirements Working Group (2006). Available at http://esto.nasa.gov/adv_planning.html 

4. Simpson Weather Associates, Charlottesville, Virginia USA. See http://www.swa.com/laser/index.html 

5. J. Yu, B. C. Trieu, E. A. Modlin, U. N. Singh, M. J. Kavaya, S. Chen, Y. Bai, P. J. Petzar, and M. Petros, “1 
J/pulse Q-switched 2-micron solid-state laser,” Opt. Letters 3 1 , 462 (2006) 

6. Yingxin Bai, Jirong Yu, Bo Trieu, Mulugeta Petros, Paul Petzar, Hyung Lee, and Upendra Singh; “Conductively 
Cooled Ho:Tm:LuLiF Laser Amplifier,” paper CTuAA2, CLEO/QELS 08, San Jose, CA, May 4-9, 2008 

7. G. J. Koch, J. Y. Beyon, B. W. Barnes, M. Petros, J. Yu, F. Amzajerdian, M. J. Kavaya, and U. N. Singh, “High- 
Energy 2-micron Doppler Lidar for Wind Measurements,” Opt. Engr. 46(1 1), 116201-1 to 116201-14 (2007)