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Advanced Earth Observation System Instrumentation Study (aeosis)Various types of measurements were studied for estimating the orbit and/or attitude of an Earth Observation Satellite. An investigation was made into the use of known ground targets in the earth sensor imagery, in combination with onboard star sightings and/or range and range rate measurements by ground tracking stations or tracking satellites (TDRSS), to estimate satellite attitude, orbital ephemeris, and gyro bias drift. Generalized measurement equations were derived for star measurements with a particular type of star tracker, and for landmark measurements with a multispectral scanner being proposed for an advanced Earth Observation Satellite. The use of infra-red horizon measurements to estimate the attitude and gyro bias drift of a geosynchronous satellite was explored.
Document ID
19770009162
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
White, R.
(Draper (Charles Stark) Lab., Inc. Cambridge, MA, United States)
Grant, F.
(Draper (Charles Stark) Lab., Inc. Cambridge, MA, United States)
Malchow, H.
(Draper (Charles Stark) Lab., Inc. Cambridge, MA, United States)
Walker, B.
(Draper (Charles Stark) Lab., Inc. Cambridge, MA, United States)
Date Acquired
September 3, 2013
Publication Date
December 1, 1975
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Report/Patent Number
NASA-CR-152418
R-965
ITR-3
Report Number: NASA-CR-152418
Report Number: R-965
Report Number: ITR-3
Accession Number
77N16105
Funding Number(s)
CONTRACT_GRANT: NAS5-21917
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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