POLE PLACEMENT WITH OUTPUT FEEDBACK.

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作者
Shapiro, E.Y.
Fredricks, D.A.
Rooney, R.H.
Barmish, B.R.
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AIRCRAFT - Control Equipment;
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摘要
A description is given of a new, application oriented, numerical procedure which allows the system designer to place the closed-loop poles using limited static output feedback. The output feedback gains, required for a particular desired closed loop pole configuration, are found via a nongradient based minimization. Algorithm description and a numerical example are provided, and the role of this new technique in the total framework of automated flight control system design is illustrated.
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