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Attitude determination by Kalman filtering.Minimum variance simulation for satellite attitude determination reliability using magnetic and solar measurements
Document ID
19670060421
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Farrell, J. L.
Date Acquired
August 3, 2013
Publication Date
September 1, 1967
Subject Category
Space Vehicles
Accession Number
67A39150
Funding Number(s)
CONTRACT_GRANT: NAS5-9195
Distribution Limits
Public
Copyright
Other
Keywords
COMPUTER SIMULATION
KALMAN-SCHMIDT FILTER
VARIANCE
MONTE CARLO METHOD
SATELLITE ATTITUDE CONTROL

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