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Microprocessor based implementation of attitude and shape control of large space structuresThe feasibility of off the shelf eight bit and 16 bit microprocessors to implement linear state variable feedback control laws and assessing the real time response to spacecraft dynamics is studied. The complexity of the dynamic model is described along with the appropriate software. An experimental setup of a beam, microprocessor system for implementing the control laws and the needed generalized software to implement any state variable feedback control system is included.
Document ID
19840016414
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Reddy, A. S. S. R. (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
84N24482
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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