文件名称:HIMAT Robust Performance Design Example
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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
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
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下载文件列表
压缩包 : HIMAT.rar 列表 HIMAT.pdf