Optimum three-dimensional flight of a supersonic aircraft |
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| Authors: | Ching-Fang Lin |
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| Institution: | Applied Dynamics International, Ann Arbor, Michigan 48104, USA |
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| Abstract: | Optimum three-dimensional flight of supersonic aircraft is considered, particularly the minimization of flight time, which is important in the climbing and turning performance of a supersonic fighter. General properties of optimum three-dimensional flight are presented, and the maximum principle is used. Optimal control is obtained by a geometrical method using the domain of manoeuvrability. |
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| Keywords: | supersonic aircraft flight performance mathematical model |
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