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Dynamics and control of flexible orbiting systemsMathematical modeling and design analysis is carried out for large flexible spacecraft and antenna systems. Modeling topics include inertially fixed attitude stabilization, solar radiation pressure effects, control systems for space mast structures, and optimal control of a hoop/column space antenna system. Each subject includes a brief overview of the pertinent literature and details of the proposed solutions for the specific modeling tasks.
Document ID
19840016413
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Bainum, P. M. (Howard Univ. Washington, DC, United States)
Pande, K. (Howard Univ. Washington, DC, United States)
Krishna, R. (Howard Univ. Washington, DC, United States)
Sivaramachandran, A. S. (Howard Univ. Washington, DC, United States)
Ananthakrishnan, S. (Howard Univ. Washington, DC, United States)
Date Acquired
August 12, 2013
Publication Date
March 22, 1984
Publication Information
Publication: NASA(Howard Univ. Large Space Structures Inst.
Subject Category
Social Sciences (General)
Accession Number
84N24481
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19840016408Collected WorksNASA/Howard University Large Space Structures Institute
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