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Issues in modeling and controlling the SCOLE configurationThe parametric study of the in-plane Spacecraft Control Laboratory Experiment (SCOLE) system, the Floquet Stability Analysis, and three dimensional formulations of the SCOLE system dynamics are examined. Control issues are discussed, such as: control of large structures with delayed input in continuous time; control with delayed input in discrete time; control law design for SCOLE using Linear Quadratic Gaussian (LQC)/TRR technique; and optimal torque control for SCOLE slewing maneuvers.
Document ID
19870008389
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bainum, Peter M. (Howard Univ., Washington, DC, United States)
Reddy, A. S. S. R. (Howard Univ., Washington, DC, United States)
Diarra, Cheick Modibo (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
87N17822
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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