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Mathematical Simulation of Flight ManeuversMathematical model simulates response of spin-stabilized spacecraft to commanded thruster pulses, using set of equations based on known inertial properties of vehicle and previously-determined thrustor performance. Model used to generate sequence of thrustor commands to accomplish specified maneuver.
Document ID
19830000644
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Frauenholz, R. B. (CALTECH)
Date Acquired
August 11, 2013
Publication Date
November 1, 1984
Publication Information
Publication: NASA Tech Briefs
Volume: 8
Issue: 2
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
NPO-15395
ISSN: 0145-319X
Report Number: NPO-15395
Accession Number
83B10644
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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