This section contains an idealized example of m-synthesis as applied to the design of a pitch axis controller of an experimental highly maneuverable airplane, HIMAT. The airplane model is taken from aerodynamic data for the HIMAT vehicle. The problem is posed as a robust performance problem, with multiplicative plant uncertainty at the plant input and plant output weighted sensitivity function as the performance criterion

Packet : HIMAT.rar filelist
HIMAT.pdf

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