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- W751390621 abstract "Control system design for general nonlinear flight dynamic models is considered through numerical simulation. The design is accomplished through a numerical optimizer coupled with analysis of flight dynamic equations. In the analysis, the general nonlinear flight dynamic equations with nonlinear aerodynamics are numerically integrated; and the dynamic characteristics needed in the optimization process are then identified from the dynamic response. To assure a reasonable solution, the initial input values of the design variables are estimated through a sensitivity analysis. To demonstrate the method, the pitch departure prevention for an F-16 configuration is demonstrated." @default.
- W751390621 created "2016-06-24" @default.
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- W751390621 date "1990-01-01" @default.
- W751390621 modified "2023-09-27" @default.
- W751390621 title "Optimal design of control systems for prevention of aircraft flight departure" @default.
- W751390621 hasPublicationYear "1990" @default.
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