NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Flight Mechanics/Estimation Theory SymposiumMethods of determining satellite orbit and attitude parameters are considered. The Goddard Trajectory Determination System, the Global Positioning System, and the Tracking and Data Relay Satellites are among the satellite navigation systems discussed. Satellite perturbation theory, orbit/attitude determination using landmark data, and star measurements are also covered.
Document ID
19800019888
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Fuchs, A. J.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1980
Subject Category
Astrodynamics
Report/Patent Number
NASA-CP-2123
Accession Number
80N28389
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available