Time-optimal aircraft pursuit evasion with a weapon envelope constraint | Zendy

P. K. Me | Zendy; Eugene L. Duke | Zendy

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Time-optimal aircraft pursuit evasion with a weapon envelope constraint

Author(s) -

P. K. Me,

Eugene L. Duke

Publication year - 1992

Publication title -

journal of guidance control and dynamics

Language(s) - English

Resource type - Journals

SCImago Journal Rank - 1.573

H-Index - 143

eISSN - 1533-3884

pISSN - 0731-5090

DOI - 10.2514/3.20856

Subject(s) - envelope (radar) , flight envelope , pursuit evasion , computer science , aeronautics , constraint (computer aided design) , evasion (ethics) , control theory (sociology) , aerospace engineering , mathematical optimization , engineering , mathematics , artificial intelligence , control (management) , aerodynamics , mechanical engineering , radar , immune system , immunology , biology

Optimal pursuit-evasion problem between two aircraft including nonlinear point-mass vehicle models and a realistic weapon envelope is analyzed. Using a linear combination of flight time and the square of the vehicle acceleration as the performance index, closed form solution is obtained in nonlinear feedback form. Due to its modest computational requirements, this guidance law useful for on-board real-time implementation.

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