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Synthesis of an Aircraft Roll-Stabilisation System: An Application of Inverse Optimal Control Theory

Published online by Cambridge University Press:  04 July 2016

B. Porter  and
M. A. Woodhead
B. Porter
Affiliation:
Department of Mechanical Engineering, University of Salford
M. A. Woodhead
Affiliation:
Department of Mechanical Engineering, University of Salford
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Extract

During the past decade, the theory of optimal control associated with linear multivariable systems having state and output equations of the respective forms

and

has been applied extensively to the design of controllers for a variety of aerospace systems. Such applications of this theory have been mainly concerned with the design of controllers that generate optimal control vectors, ẑ, which minimise performance indices of the form.

where Q and R are positive-definite matrices.

Type
Technical notes
Information
The Aeronautical Journal , Volume 74 , Issue 713 , May 1970 , pp. 390 - 392
Copyright
Copyright © Royal Aeronautical Society 1970 

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References

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