A multivariable synthesis procedure based on eigenvalue/eigenvector assignment is reviewed and is employed to develop a systematic design procedure to meet the lateral handling qualities design objectives of a fighter aircraft over a wide range of flight conditions. The closed loop modal characterization developed provides significant insight into the design process and plays a pivotal role in the synthesis of robust feedback systems. The simplicity of the synthesis algorithm yields an efficient computer aided interactive design tool for flight control system synthesis.
Modal control theory and application to aircraft lateral handling qualities design
1978-06-01
Report
Keine Angabe
Englisch
Preliminary aircraft design: lateral handling qualities
Online Contents | 2001
|TIBKAT | 1999
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