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Controllability of inherently damped large flexible space structuresGraph theoretic techniques are used to study controllability of linear systems which represent large flexible orbiting space systems with inherent damping. The controllability of the pair of matrices representing the system state and control influence matrices is assured when all states in the model are reachable in a digraph sense from at least one input and also when the term rank of a Boolean matrix whose non trivial components are based on the state and control influence matrices has a term rank of the order of the state vector. The damping matrix does not influence the required number of actuators but gives flexibility to the possibility locations of the actuators for which the system is controllable.
Document ID
19820020469
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Reddy, A. S. S. R.
(Howard Univ. Washington, DC, United States)
Bainum, P. M.
(Howard Univ. Washington, DC, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1982
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-CR-169127
IAF-82-319
NAS 1.26:169127
Report Number: NASA-CR-169127
Report Number: IAF-82-319
Report Number: NAS 1.26:169127
Accession Number
82N28345
Funding Number(s)
CONTRACT_GRANT: NSG-1414
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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