For the issue of determination of flight range of controlled aircraft, under the condition of given constrained control, linear differential movement equations of aircraft are chosen and solved in a comparatively short time to determine the flight range based on maximum principle in modern optimizing control theory. The example illustrates that calculation accuracy is high, and the proposed method is effective and feasible and also has reference value for engineering application.
Application of Optimizing Control in Determining Flight Range of Aircraft
2010
4 Seiten, 4 Quellen
Aufsatz (Konferenz)
Englisch
Optimizing aircraft performance with adaptive, integrated flight/propulsion control
Tema Archiv | 1990
|Optimizing aircraft performance with adaptive, integrated flight/propulsion control
Tema Archiv | 1991
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