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• W2321850820 abstract "Multivariable control laws for the lateral axis of a fighter aircraft operating a t subsonic speeds are presented. A feedback gain matrix, designed using linear quadratic regulator theory with integral action, is used to track stability axis roll r a t e a n d sideslip angle commands. The design weights for the LQ regulator are chosen to produce desirable flying qualities. The closed loop aircraft meets flying qualities specifications across the subsonic flight envelope. The control laws are realized in a nonlinear simulation by scheduling the regulator gains with dynamic p r e s su re us ing a cubic he rmi t e interpolation. This design forms the basis for control laws a t high angles of" @default.
• W2321850820 created "2016-06-24" @default.
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• W2321850820 date "1992-08-10" @default.
• W2321850820 modified "2023-09-27" @default.
• W2321850820 title "Control law development for the lateral axis of a fighter aircraft" @default.
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• W2321850820 doi "https://doi.org/10.2514/6.1992-4408" @default.
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