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Autonomous Orbital Calculation for SatellitesOnboard orbital navigation system reduces dependence on Earth-tosatellite links. Report discusses mathematics of proposed navigation subsystem that keeps geostationary satellite in proper orbit without ground control. Subsystem uses data from Earth and Sun sensors to activate thrusters for station-keeping maneuvers. With sensors already on satellites for determining attitude, subsystem maintains satellite within 3 degrees of specified equatorial longitude for up to 6 months. With more accurate sensors, subsystem able to maintain orbit within 0.1 degrees.
Document ID
19860000305
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Mease, K. D.
(Caltech)
Ryne, M. S.
(Caltech)
Wood, L. J.
(Caltech)
Date Acquired
August 12, 2013
Publication Date
May 1, 1986
Publication Information
Publication: NASA Tech Briefs
Volume: 10
Issue: 3
ISSN: 0145-319X
Subject Category
Mathematics And Information Sciences
Report/Patent Number
NPO-16532
ISSN: 0145-319X
Report Number: NPO-16532
Accession Number
86B10305
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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