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Time-optimal bang-bang slew of rigidized SCOLE configurationThis paper addresses: (1) an application of the well-known time-optimal bang-bang control theory to the design of minimal-time limited-torque single-axis slew maneuvers for the rigidized configuration of NASA Langley Research Center's Spacecraft Control Laboratory Experiment (SCOLE) and (2) the associated generic side effects due to spillover of slew motions and applied torques. Numerical experiments that helped pinpoint the specific causes of performance degradation are discussed. Analytical as well as scientifically interesting numerical research results are given.
Document ID
19850022851
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lin, J. G. (Northeastern Univ. Boston, United States)
Taylor, L. W., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
April 1, 1985
Publication Information
Publication: JPL Proc. of the Workshop on Identification and Control of Flexible Space Struct., Vol. 1
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
85N31164
Funding Number(s)
CONTRACT_GRANT: NAG1-386
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19850022835Collected WorksProceedings of the Workshop on Identification and Control of Flexible Space Structures, volume 1
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