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Optimal torque control for SCOLE slewing maneuversThe Spacecraft Control Laboratory Experiment (SCOLE) was slewed from one attitude to the required attitude and an integral performance index which involves the control torques was minimized. Kinematic and dynamical equations, optimal control, two-point boundary-value problems, and estimation of unknown boundary conditions are presented.
Document ID
19870008390
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bainum, P. M. (Howard Univ., Washington, DC, United States)
Li, Feiyue (Howard Univ., Washington, DC, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1987
Publication Information
Publication: NASA. Langley Research Center Proceedings of the 3rd Annual SCOLE Workshop
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
87N17823
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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