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A Mathematical Formulation of the SCOLE Control Problem. Part 2: Optimal Compensator DesignThe study initiated in Part 1 of this report is concluded and optimal feedback control (compensator) design for stability augmentation is considered, following the mathematical formulation developed in Part 1. Co-located (rate) sensors and (force and moment) actuators are assumed, and allowing for both sensor and actuator noise, stabilization is formulated as a stochastic regulator problem. Specializing the general theory developed by the author, a complete, closed form solution (believed to be new with this report) is obtained, taking advantage of the fact that the inherent structural damping is light. In particular, it is possible to solve in closed form the associated infinite-dimensional steady-state Riccati equations. The SCOLE model involves associated partial differential equations in a single space variable, but the compensator design theory developed is far more general since it is given in the abstract wave equation formulation. The results thus hold for any multibody system so long as the basic model is linear.
Document ID
19890005792
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Balakrishnan, A. V.
(California Univ. Los Angeles, CA, United States)
Date Acquired
September 5, 2013
Publication Date
December 1, 1988
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-CR-181720
NAS 1.26:181720
Report Number: NASA-CR-181720
Report Number: NAS 1.26:181720
Accession Number
89N15163
Funding Number(s)
PROJECT: RTOP 585-01-51-01
CONTRACT_GRANT: NAG1-464
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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