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Validation of the Galileo scan platform control design using DISCOSThe flexibility of the Galileo spacecraft's scan platform control system stator structure, which lies between the scan platform and one of the control actuators, has been a major design consideration. Tests have been conducted to verify the prevention of undesirable interactions between the structure and the control loop, by means of the Dynamic Interaction Simulation of Controls and Structure (DISCOS) program. The scan platform's control design has been validated for the achievement of 140-microradians maximum position deviation and 50 microradians of jitter over 1-sec intervals.
Document ID
19840060689
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chodas, J. L.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Macala, G. A.
(California Institute of Technology, Jet Propulsion Laboratory, Guidance and Control Section, Pasadena CA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1984
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 84-1964
Accession Number
84A43476
Funding Number(s)
CONTRACT_GRANT: NAS5-11996
Distribution Limits
Public
Copyright
Other

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