Satellite laser ranging

Source: Wikipedia, the free encyclopedia.
(Redirected from
International Laser Ranging Service
)
This article is about the up-looking type of satellite laser. For the down-looking type, see
Satellite laser altimetry
.
Laser Ranging System of the geodetic observatory Wettzell, Bavaria

In satellite laser ranging (SLR) a global network of observation stations measures the round trip time of flight of ultrashort pulses of light to satellites equipped with retroreflectors. This provides instantaneous range measurements of millimeter level precision which can be accumulated to provide accurate measurement of orbits and a host of important scientific data. The laser pulse can also be reflected by the surface of a satellite without a retroreflector, which is used for tracking space debris.[1]

Satellite laser ranging is a proven geodetic technique with significant potential for important contributions to scientific studies of the earth/atmosphere/ocean system. It is the most accurate technique currently available to determine the geocentric position of an Earth satellite, allowing for the precise calibration of radar altimeters and separation of long-term instrumentation drift from secular changes in ocean topography.

Its ability to measure the variations over time in Earth's gravity field and to monitor motion of the station network with respect to the geocenter, together with the capability to monitor vertical motion in an absolute system, makes it unique for modeling and evaluating long-term climate change by:[2]

  • providing a reference system for post-glacial rebound, plate tectonics, sea level and ice volume change[3]
  • determining the temporal mass redistribution of the solid earth, ocean, and atmosphere system[4]
  • determining Earth orientation parameters, such as Earth pole coordinates and length-of-day variations[5]
  • determining of precise satellite orbits for artificial satellites with and without active devices onboard[6][7]
  • monitoring the response of the atmosphere to seasonal variations in solar heating.[8]

SLR provides a unique capability for verification of the predictions of the theory of general relativity, such as the frame-dragging effect.

SLR stations form an important part of the international network of

DORIS
and PRARE systems. On several critical missions, SLR has provided failsafe redundancy when other radiometric tracking systems have failed.

History

Satellite Laser Ranging

Laser ranging to a near-Earth satellite was first carried out by NASA in 1964 with the launch of the Beacon-B satellite. Since that time, ranging precision, spurred by scientific requirements, has improved by a factor of a thousand from a few metres to a few millimetres, and more satellites equipped with retroreflectors have been launched.

Several sets of retroreflectors were installed on Earth's

lunar laser ranging
), providing a highly accurate measurement of the dynamics of the Earth/Moon system.

During the subsequent decades, the global satellite laser ranging network has evolved into a powerful source of data for studies of the solid Earth and its ocean and atmospheric systems. In addition, SLR provides

precise orbit determination
for spaceborne radar altimeter missions mapping the ocean surface (which are used to model global ocean circulation), for mapping volumetric changes in continental ice masses, and for land topography. It provides a means for subnanosecond global time transfer, and a basis for special tests of the Theory of General Relativity.

The International Laser Ranging Service was formed in 1998[9] by the global SLR community to enhance geophysical and geodetic research activities, replacing the previous CSTG Satellite and Laser Ranging Subcommission.

Applications

SLR data has provided the standard, highly accurate, long wavelength gravity field reference model which supports all precision orbit determination and provides the basis for studying temporal gravitational variations due to mass redistribution. The height of the geoid has been determined to less than ten centimeters at long wavelengths less than 1,500 km.

SLR provides mm/year accurate determinations of tectonic drift station motion on a global scale in a geocentric reference frame. Combined with gravity models and decadal changes in Earth rotation, these results contribute to modeling of convection in the Earth's mantle by providing constraints on related Earth interior processes. The velocity of the fiducial station in Hawaii is 70 mm/year and closely matches the rate of the background geophysical model.

List of satellites

List of passive satellites

For broader coverage of this topic, see List of passive satellites.

Several dedicated laser ranging satellites were put in orbit:[10]

List of shared satellites

Several satellites carried laser retroreflectors, sharing the bus with other instruments:

See also

References

  1. doi:10.1002/2017EA000329
    .
  2. S2CID 127408940
    .
  3. doi:10.1007/s00190-019-01307-0
    .
  4. ^
    doi:10.1007/s00190-015-0825-1
    .
  5. doi:10.1186/s40623-019-1000-3
    .
  6. doi:10.1007/s00190-018-1143-1
    .
  7. S2CID 125791718
    .
  8. S2CID 127713034
    .
  9. S2CID 127335882
    .
  10. ^ "International Laser Ranging Service". Ilrs.gsfc.nasa.gov. Retrieved 2022-08-20.
  11. S2CID 191188229
    .
  12. ^ "Calsphere 1, 2, 3, 4". Space.skyrocket.de. Retrieved 2016-02-13.
  13. ^ Lindborg, Christina. "Etalon". Russia and Navigation Systems. Federation of American Scientists. Retrieved 10 November 2012.
  14. doi:10.1515/acgeo-2015-0032
    .
  15. doi:10.1515/arsa-2015-0001
    .
  16. ^ "Larets".
  17. ^ "International Laser Ranging Service". Ilrs.gsfc.nasa.gov. Retrieved 2022-08-20.
  18. ^ "NASA - NSSDCA - Spacecraft - Details". Nssdc.gsfc.nasa.gov. 1999-06-05. Retrieved 2016-02-13.
  19. S2CID 121163799
    .
  20. ^
    S2CID 127408940
    .
  21. S2CID 125791718
    .
  22. doi:10.1007/s10291-020-01026-6
    .
  23. doi:10.1007/s00190-015-0810-8
    .
  24. doi:10.1007/s00190-017-1050-x
    .
  25. doi:10.1007/s10291-020-0965-5
    .
  26. ^ "IRNSS: Reflector Information". ilrs.cddis.eosdis.nasa.gov. Archived from the original on 2019-03-25. Retrieved 2019-03-25.
  27. S2CID 134160047
    .
  28. doi:10.3390/rs11192282
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  29. ISBN 9781510616196
    .

Further reading

External links

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