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Analysis and Simulation of the Mariner Mars 1971 Scan Platform: Spacecraft Dynamic InteractionThe equations of motion are developed which describe the dynamic interaction between the spacecraft bus and the movable appendages about a single axis. The effect is evaluated of the dynamic interaction on the attitude control subsystem with computer simulations, and design recommendations to reduce the impact of this interaction on future attitude control subsystems are presented.
Document ID
19730022105
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Schumacher, L.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 2, 2013
Publication Date
August 15, 1973
Subject Category
Space Vehicles
Report/Patent Number
NASA-CR-133793
JPL-TM-33-624
Report Number: NASA-CR-133793
Report Number: JPL-TM-33-624
Accession Number
73N30837
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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