Technique of dynamic programming is used to determine optimum flight profiles for interceptor aircraft; future development resulted in ground-based computer program which outputs printed graphical presentation of families of profiles; visual display performs variety of functions, particularly those involving problems of selecting general flight control laws and logic to be designed into airborne flight control computers; tactical situations are analyzed.
Graphic presentation of optimum flight profiles
Aero/Space Eng
Aerospace Engineering ; 19 , n 9 ; p 16-17 + 46
1960
Article (Journal)
English
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