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Performance analysis of the Spaceborne Laser Ranging SystemThe performance of the Spaceborne Laser Ranging System in the determination of distances between ground-based targets is discussed. The system consists of an orbiting pulsed laser distance measurement system that sequentially measures the distance to retroreflector arrays on the ground. Intersite distances are then determined from an analysis of the vertical distance data and the spacecraft orbital dynamics. Results of computer simulations indicate that for a six-day observing period with 50 percent cloud cover, uncertainties of 1 to 3 cm are expected for intertarget separations of 50 to 1200 km, with vertical uncertainties from 1 to 12 cm. Furthermore, it is found that by redetermining relative target positions, precision can be increased to less than 0.3 cm to 1 cm in the baseline and to 0.4 to 4 cm in vertical distance. It is concluded that with these precisions, strain and strain rate can be determined for crustal dynamics and earthquake studies, and geodetic surveys can be performed.
Document ID
19800062404
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Kahn, W. D.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Vonbun, F. O.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Smith, D. E.
(NASA Goddard Space Flight Center Greenbelt, Md., United States)
Englar, T. S.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Gibbs, B. P.
(Business and Technological Systems, Inc. Seabrook, Md., United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1980
Publication Information
Publication: Bulletin Geodesique
Volume: 54
Issue: 2, 19
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Accession Number
80A46574
Distribution Limits
Public
Copyright
Other

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