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Quasi-optimum design of a six degree of freedom moving base simulator control systemThe design of a washout control system for a moving base simulator is treated by a quasi-optimum control technique. The broad objective of the design is to reproduce the sensed motion of a six degree of freedom simulator as accurately as possible without causing the simulator excursions to exceed specified limits. A performance criterion is established that weights magnitude and direction errors in specific force and in angular velocity and attempts to maintain the excursion within set limits by penalizing excessive excursions. A FORTRAN routine for relizing the washout law was developed and typical time histories using the washout routine were simulated for a range of parameters in the penalty- and weighting-functions. These time histories and the listing of the routine are included in the report.
Document ID
19740002186
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Friedland, B.
(Singer Co. Little Falls, NJ, United States)
Ling, C.
(Singer Co. Little Falls, NJ, United States)
Hutton, M. F.
(Singer Co. Little Falls, NJ, United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1973
Publication Information
Publisher: NASA
Subject Category
Facilities, Research, And Support
Report/Patent Number
NASA-CR-2312
Report Number: NASA-CR-2312
Accession Number
74N10299
Funding Number(s)
CONTRACT_GRANT: NAS2-3636
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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