Path: Common/Control
% Apply eigenvector assignment using the Draper method.
vD is entered with nan where you don't care about the value of the
eigenvector.
Type EAssignDraper for a demo.
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Form:
f = ESAssignDraper( g, lambda, vD, r, fC )
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Inputs
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g (:) State space system of type statespace
lambda (n) Desired eigenvalues
vD (:,n) Desired eigenvectors
r (:,n) Weighting matrix
fC (3,p) Control constraint equation
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Outputs
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f Gain matrix
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Reference: Orr H. A., "An Integrated Fire/Flight Control System for
a Conventionally Configured A-10 Aircraft," CSDL-T-794,
December 1982.
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