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A computerized compensator design algorithm with launch vehicle applications

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2 Author(s)
J. Mitchell ; Mississippi State University, Mississippi State, MS, USA ; W. McDaniel

This short paper presents a computerized algorithm for the design of compensators for large launch vehicles. The algorithm is applicable to the design of compensators for linear, time-invariant, control systems with a plant possessing a single control input and multioutputs. The achievement of frequency response specifications is cast into a strict constraint mathematical programming format. An improved solution algorithm for solving this type of problem is given, along with the mathematical necessities for application to systems of the above type. A computer program, compensator improvement program (CIP), has been developed and applied to a pragmatic space-industry-related example.

Published in:

IEEE Transactions on Automatic Control  (Volume:21 ,  Issue: 3 )