th ams annual meeting - nasa · 95th ams annual meeting january 8, 2015 ... backup slides 17. drs...

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Technology Advancement for Active Remote Sensing of Carbon Dioxide from Space using the ASCENDS CarbonHawk Experiment Simulator (ACES): First Results M. Obland 1 , A. Nehrir 1 , J. Campbell 1 , J. Dobler 2 , T. Zaccheo 3 , F. Harrison 1 , S. Kooi 4 , B. Lin 1 , Y. Choi 2 , J. Plant 1 , M. Yang 1 , C. Antill 1 , S. Ismail 1 , E. Browell 5 , B. Meadows 1 , B. Moore 6 , S. Crowell 6 1 NASA Langley Research Center (LaRC) 2 Exelis Inc. 3 Atmospheric and Environmental Research (AER) 4 Science Systems and Applications, Inc. (SSAI) 5 STARSSII Affiliate, NASA LaRC 6 University of Oklahoma 95 th AMS Annual Meeting January 8, 2015 https://ntrs.nasa.gov/search.jsp?R=20160006921 2020-06-21T09:42:07+00:00Z

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Page 1: th AMS Annual Meeting - NASA · 95th AMS Annual Meeting January 8, 2015 ... Backup Slides 17. DRS Technologies HgCdTe array • ~4.9 MHz bandwidth @ gain of 10^6 • Continuously

Technology Advancement for Active Remote Sensing of Carbon Dioxide from Space using the ASCENDS CarbonHawk

Experiment Simulator (ACES): First Results

M. Obland1, A. Nehrir1, J. Campbell1, J. Dobler2, T. Zaccheo3, F. Harrison1, S. Kooi4, B. Lin1, Y. Choi2, J. Plant1, M. Yang1, C. Antill1, S. Ismail1, E. Browell5, B. Meadows1, B. Moore6, S. Crowell6

1NASA Langley Research Center (LaRC)2Exelis Inc.

3Atmospheric and Environmental Research (AER)4Science Systems and Applications, Inc. (SSAI)

5STARSS‐II Affiliate, NASA LaRC6University of Oklahoma

95th AMS Annual Meeting

January 8, 2015

https://ntrs.nasa.gov/search.jsp?R=20160006921 2020-06-21T09:42:07+00:00Z

Page 2: th AMS Annual Meeting - NASA · 95th AMS Annual Meeting January 8, 2015 ... Backup Slides 17. DRS Technologies HgCdTe array • ~4.9 MHz bandwidth @ gain of 10^6 • Continuously

The ASCENDS CarbonHawk Experiment Simulator (ACES) is an Instrument Incubator Program (IIP) project that seeks to advance technologies critical to measuring atmospheric column carbon 

dioxide (CO2) mixing ratios from space in support of the ASCENDS (Active Sensing of CO2 Emissions over Nights, Days, and Seasons) 

Decadal Survey mission:

• Passive satellite measurements cannot make retrievals of CO2column densities to the surface at night, at high latitudes (i.e. northern Europe during winter and over the poles), and through cirrus clouds, high optical depth aerosols, or in presence of scattered clouds.

• Active measurements using lidars do not have these limitations, and they can therefore fill these data gaps and aid in the refinement and understanding of the global carbon cycle budget.

ACES Scientific Motivation

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– Simultaneously transmits multiple wavelengths (on / off) reducing atmospheric noise & eliminating surface reflectance variations.

– Approach is independent of the system wavelength and allows simultaneous CO2 & O2 (1.26 m) measurements for deriving mixing ratio (XCO2).

Line-Center Side-Line

(+10 pm) Off-Line-1 (+50 pm)

Off-Line-2 (-50 pm)

1.57‐m CO2 Measurement Architecture

Dobler, et al., Applied Optics, 2013

ACES architecture based on Exelis Multi-functional Fiber Laser Lidar (MFLL):

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Intensity‐Modulated Continuous‐Wave (IM‐CW) Measurement Technique

Progression of Transmitted and Received Intensity‐Modulated Waveforms

Simultaneously‐transmitted intensity modulated range 

encoded waveforms

Simultaneously‐received Online and Offline IPDA returns

Measurement: Output of correlation between 

transmitted and received waveforms

Range

Pon

Poff

Range‐encoded approach for detection and ranging is analogous to mature Frequency‐Modulated Continuous Wave (FM‐CW) Radar and GPS 

measurement techniques  

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ACES is advancing 4 key technology areas:(1)Enable development of more advanced modulation waveforms with 

improved detector subsystem

(2) Increase transmit power and efficiency for CO2 measurements at 1.57 microns using commercial amplifiers with stable, tunable laser‐line locking system 

(3) Demonstrate column CO2 retrievals with alignment of multiple laser beams transmitting simultaneously in the far‐field for scalability to space

(4) Continue refining CO2 column retrieval algorithms in the presence of low optical depth clouds and distributed scattering layers (i.e. aerosol layers)

Technology Challenges

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July 1July 7July 8aJuly 8bJuly 13July 16

NASA Langley Research Center

Flight Summary: 17.4 flight hours

Data recorded at multiple altitudes over land and ocean surfaces with and without intervening clouds.

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July 1July 7July 8aJuly 8bJuly 13July 16

NASA Langley Research Center

Data recorded at multiple altitudes over land and ocean surfaces with and without intervening clouds.

50 ft. low approach into Ahoskie, NC, airport

Flight Summary: 17.4 flight hours

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Preliminary Results: Combination of Multiple Transmitters

13) All EDFAs 14) EDFAs 1+2 15) EDFA 1

Bias from combination of multiple beams in far field is small (<1%) if present at all

0.4%change 1%

change

0.5%precision 0.8%

precision

Altitude = 30,000 ft

Major question for scalability to spaceflight is whether combining individual transmit beams in far field induces a bias in the measurements.• Initial data show only small changes in measurements – about 1% on average – which could

be due to beam combination bias, calibration drift, aircraft attitude, or natural variability.

Cloud!

Signal dropout over calm ocean surface

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Preliminary Results: Combination of Multiple Transmitters

13) All EDFAs 14) EDFAs 1+2 15) EDFA 1

Bias from combination of multiple beams in far field is small (<1%) if present at all

0.4%change 1%

change

0.5%precision 0.8%

precision

Altitude = 30,000 ft

Major question for scalability to spaceflight is whether combining individual transmit beams in far field induces a bias in the measurements.• Initial data show only small changes in measurements – about 1% on average – which could

be due to beam combination bias, calibration drift, aircraft attitude, or natural variability.

Cloud!

Signal dropout over calm ocean surface

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James River

RushmereRiver Cliff Hampton VA Chesapeake 

Bay Bridge

Preliminary Results: Ranging

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James River

RushmereRiver Cliff Hampton VA Chesapeake 

Bay Bridge

Chesapeake Bay Bridge (100 Hz)

Preliminary Results: Ranging

IM-CW technique accurately retrieves range over a variety of surfaces and in the presence of optically thin clouds allowing for retrievals of column CO2

mixing ratios to surface and cloud tops.

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• Advanced deconvolution techniques resolve cloud and forest features:– Fourier transform reordering (Interpolated profile)– Richardson-Lucy deconvolution (Enhanced profile)

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Preliminary Results: Ranging

Thin Cirrus

GroundReturn

Vegetation canopy height & thickness

IM-CW technique accurately retrieves range over a variety of surfaces and in the presence of optically thin clouds allowing for retrievals of column CO2

mixing ratios to surface and cloud tops.

Campbell, et al., Optics Express, 2014

Campbell, et al., Optics Letters, 2014

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Preliminary CO2 Retrievals:Ocean and Land

• CO2 retrieval values (2‐s average) are calibrated using primary and secondaryoffline wavelengths

• Average of in situ data across entire flight (binned by altitude) used for comparisons

• Actual CO2 number densities likely different far away from spiral point and airport

• Further work is needed to compare directly with data from in situ spirals

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Summary

• The ACES team is advancing technologies critical to making CO2column mixing ratio measurements from space.– HgCdTe detector/TIA bandwidth increased to ~4.9 MHz for advanced

modulation waveforms– Increased transmitter power and receiver aperture yielding high precision

measurements over varying surfaces• ACES recorded meaningful data at multiple altitudes over land and

ocean surfaces, with and without intervening clouds during its first test flights.– Preliminary data show excellent range retrievals that can produce cloud and

vegetation canopy structures using advanced deconvolution techniques– Initial CO2 retrievals show reasonable agreement (~1 ppm) compared with in

situ measurements over water; over land measurements need more study• Data analysis, comparisons, and technology advancement efforts

are continuing.14

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Future Directions

• Continue data analysis to fully quantify instrument performance

• Continue flight testing of new modulation algorithms and hardware improvements– Deconvolution techniques for clouds and forest canopies– Operational tests of retrievals with sideline wavelengths– Instrument automation for UAV operations

• Continue Technology Readiness Level (TRL) advancement and space qualification of ASCENDS technologies– Example: Small Business Innovation Research project with

Fibertek for laser amplifier advancement

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AcknowledgementsThank you to the NASA Earth Science Technology Office

(ESTO) for funding this project and to the NASA Headquarters ASCENDS Program and NASA Langley for additional support.

• The authors wish to thank the many contributions to this work from the restof the ACES team at Exelis (Douglas McGregor, Nathan Blume, MichaelBraun, Mark Shure, Mark Neal, Joe Bender, Steve Horney), WelchMechanical Designs (Wayne Welch), Oklahoma University (Berrien Moore,Sean Crowell), the University of Melbourne (Peter Rayner), NP Photonics(Arturo Chavez-Pirson), NASA Langley (Chuck Antill, Michael Kissam,Melissa Yang, Jim Plant, Yonghoon Choi, Narasimha Prasad, Keith Murray,Tony Notari, Craig Cleckner, John Barrick, Ali Aknan, Janet Dail, Carl Mills,Chris Herdey, Rebecca Stavely, Nick Vitullo, Marie Avery), and the aircraftsupport teams at Langley and Armstrong Flight Research Center.

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Backup Slides

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DRS Technologies HgCdTe array• ~4.9 MHz bandwidth @ gain of 10^6• Continuously cooled at 77 K• NEP: 2.4 fW/Hz1/2

• Excess Noise Factor: ~1.1• Tested with MFLL on DC-8 in 2013Transmitters:• Three Erbium-Doped Fiber Amplifiers (each

10 W average, 20 W peak) locked to CO2absorption line (1.57 microns)

• Wavelength tunable within +/- 50 pm (6 GHz) from line center

Combination of low-noise detector, higher power transmitters, and larger collection apertures improves signal-to-noise ratio; increased bandwidth allows

for use of more advanced modulation waveforms.

Transmitters and Telescopes

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July 1July 7July 8aJuly 8bJuly 13July 16

NASA Langley Research Center

Data recorded at multiple altitudes over land and ocean surfaces with and without intervening clouds.

Typical cloud conditions

50 ft. low approach into Ahoskie, NC, airport

Flight Summary: 17.4 flight hours