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An Indepth Look at ICESat and GLAS

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Title: An Indepth Look at ICESat and GLAS


1
An In-depth Look at ICESat and GLAS
  • By Vishana Ramdeen

2
Abstract
  • The ICESat (Ice, Cloud, and land Elevation
    Satellite) spacecraft was launched on January 12,
    2003 into a near-circular, low Earth,
    Sun-Synchronous Orbit with a 94? inclination.
    Its objective is to quantify the mass balance of
    the polar ice sheets and observe the changes with
    time. The only scientific observation instrument
    onboard is the GLAS (Geoscience Laser Altimeter
    System) instrument. It consists of three lasers
    (Laser 1, 2, and 3) which operate one at a time
    for three 33-day campaigns per year. GLASs
    Lasers 1 and 2 experienced a rapid decrease in
    laser energy which was attributed to issues with
    the frequency doubler, a manufacture defect of
    the laser diode pump array, and trace levels of
    outgassing. One of the major shortcomings of
    ICESat is systematic pointing errors. Two of the
    calibration methods used to compensate for these
    errors are ocean scans and round the world
    scans. The ICESat has provided scientists with
    information that is unsurpassed by any existing
    satellite and expectations for the future are
    high.

3
Agenda
  • Introduction
  • Overview of the physical instruments
  • ICESat
  • GLAS
  • General and Orbital Characteristics
  • GLAS Lasers
  • Shortcomings
  • solutions
  • Conclusion

4
Introduction
  • ICESat Ice, Cloud, and land Elevation Satellite
  • Launched into orbit on January 12, 2003 on a
    Boeing Delta II rocket from the Vandenberg Air
    Force Base in California

5
Introduction
  • Inclination 94?
  • Retrograde Orbit
  • Near circular, low Earth orbit
  • Sun-Synchronous Orbit
  • Altitude 590 km initially
  • currently at 600 km
  • Orbital period 96.6 minutes
  • Two reference tracks 8-day exact repeat (for
    calibration purposes) and 91-day exact repeat
    (for denser track coverage)

6
ICESat
Schutz et al. ICESat Overview
7
ICESats Mission Objectives
  • The primary goal of ICESat is to quantify ice
    sheet mass balance and understand how changes in
    the Earths atmosphere and climate affect polar
    ice masses and global sea level.
  • Measures height profiles of clouds, aerosols
    distribution, vegetation cover, and land
    elevations.

8
ICESat/GLAS
  • ICESat (zenith view)

  • GLAS

www.csr.utexas.edu/glas and glas.gsfc.nasa.gov
9
GLAS
  • GLAS Geoscience Laser Altimeter System
  • First LIDAR used for continuous global
    observations of the Earth
  • A combination of a precision surface LIDAR with a
    sensitive dual-wavelength cloud and aerosol LIDAR
  • Only scientific observational instrument on the
    ICESat spacecraft

10
GLAS
  • Consists of three lasers
  • referred to as Lasers 1, 2, and 3
  • Mounted on a stationary optical bench
  • Laser measurement direction is nadir, but the
    spacecraft can perform roll maneuvers to point up
    to 5 off nadir
  • Only one laser is in operation at a time, pulsing
    at 40 Hz
  • Pulse width is 5 nanometers

11
GLAS Lasers
Abshire et al. Geoscience Laser Altimeter System
(GLAS)
  • Each pulse has an averaged 65 m footprint
  • successive laser pulses spaced 172 m along-track
  • Area on the Earths surface covered by each pulse
    is not equal
  • Lasers far field patterns are hypothesized to
    change due to the change of spatial distribution
    of light from the laser diode pump arrays over
    time more generally with laser energy and time
  • laser diode pumps are used to produce very high
    power outputs such as that used for GLASs
    continuous pulses

12
GLAS Lasers
Abshire et al. Geoscience Laser Altimeter System
(GLAS)
  • 2 out of the 3 lasers experienced more rapid
    energy loss than planned
  • After the first 10 days Laser 1s transmitted
    energy began to rapidly decline
  • by day 38 it completely failed
  • caused by manufactures defect of laser diode
    pump array
  • To counter the effects of having less lasers,
    ICESats duty cycle was reduced from 100 to 25
  • Lasers 2 and 3 are operating for three 33-day
    campaigns per year (Campaigns a, b, and c)
  • Laser 2s decline is attributed to a process
    related to the frequency doubler and trace levels
    of outgassing.
  • To slow this fate, Laser 3 has been operating at
    a lower energy level

13
Coverage?
  • http//en.wikipedia.org/wiki/ICESat

14
Hows it done?
  • GLAS emits a 1064 nm (for surface and cloud tops)
    and 532 nm (for atmospheric aerosols) laser pulse
    toward Earths surface.
  • time emitted is recorded
  • Upon impact to a surface, the photons are
    scattered back to the satellite.
  • When the photons come into contact with the
    receiver another timestamp is taken.
  • measurements of time of flight, emission angle
    relative to inertial space, transmitted pulse
    waveform, and echo pulse waveform are taken
  • the time of flight is divided by 2 and multiplied
    by the speed of light giving us the distance

http//www.nasa.gov/vision/earth/lookingatearth/ic
esat_billion.html
15
Backscatter
  • Strong echo pulses indicate a region of flat,
    bright ice
  • 532 nm profiles (B) have better signal-to-noise
    ratios for weak aerosol backscatter because of
    their more sensitive photon counting detectors

A
B
Abshire et al. Geoscience Laser Altimeter System
(GLAS)
16
An Example
  • http//earthobservatory.nasa.gov/Library/ICESat/Im
    ages/greenland_icesheet.jpg

17
Shortcomings
  • Systematic pointing errors are preventing ICESat
    data from meeting its full potential
  • long-term trend bias
  • systematic variations with satellite orbital
    period revolution
  • These errors create elevation errors in the data
    and change with time
  • They pose problems since they are indiscernible
    from actual surface elevation change

18
Can we fix it?
  • Ocean scans
  • performed twice a day over the mid-Pacific
  • errors are estimated through the reduction of the
    ocean surface range deviations from each ocean
    scan
  • Round the world scans
  • performed every 8 days
  • estimates the systematic pointing errors as a
    function of orbital angle

19
ICESat Video
http//www.nasa.gov/mission_pages/icesat/
Note To see this video, go to the above website
and click on the second video from the top.
20
Conclusion
  • The ICESat has provided scientists with
    unprecedentedly accurate data of the globes
    polar regions. With the addition of a few
    calibrations the usefulness of its outputs would
    grow increasingly.

21
References
  • Abshire, J., et al. (2005), Geoscience Laser
    Altimeter System (GLAS) on the ICESat Mission
    On-orbit measurement performance, Geophysical
    Research Letter, doi10.1029/2005GL024028,
    1534-1536.
  • ICESat (2008). In Wikipedia, The Free
    Encyclopedia. Retrieved 0537, May 7, 2008, from
    http//en.wikipedia.org/w/index.php?titleICESato
    ldid182396442.
  • Luthcke, S. B., D. D. Rowlands, T. A. Williams,
    and M. Sirota (2005), Reduction of ICESat
    systematic geolocation errors and the impact on
    ice sheet elevation change detection, Geophysical
    Research Letters, 32, L21S05, doi10.1029/2005GL02
    3689.
  • Schutz, B. E., H. J. Zwally, C. A. Shuman, D.
    Hancock, and J. P. DiMarzio (2005), Overview of
    the ICESat Mission, Geophysical Research Letters,
    32, L21S01, doi10.1029/2005GL024009.
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