A study of three-dimensional, minimum-time turning maneuvers for supersonic fighter aircraft is described. For turns which do not specify the end-point position, the optimum maneuvers comprise a one-parameter family of flight paths. All the optimum turns, and their associated control variables can be presented in simple graphical form for a specified aircraft configuration. A feedback control diagram can be easily constructed for all minimum-time turns to a specified final energy level. This feedback chart could be implemented in the airborne computer to provide real-time, on-line optimal flight path control. Numerical results for an early model of the F4 fighter illustrate the control technique. (Author)
A Study of Techniques for Real-Time, On-Line Optimum Flight Path Control. Three-Dimensional Minimum-Time Flight Paths with Two State Variables
1974
37 pages
Report
No indication
English
Engineering Index Backfile | 1960
|Engineering Index Backfile | 1959
|TIBKAT | 1959
|NTIS | 1959
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