Guidelines for developing a multivariable centralized automatic flight control system (AFCS) for a twin lift helicopter system (TLHS) are presented. Singular value ideas are used to formulate performance and stability robustness specifications. A linear Quadratic Gaussian with Loop Transfer Recovery (LQG/LTR) design is obtained and evaluated.
Multivariable control of a twin lift helicopter system using the LQG/LTR design methodology
1986-01-01
Report
Keine Angabe
Englisch
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