A Initial Trajectory Planning Based on Genetic Algorithm for Short Range Air to air Missile
Yang Chen
Abstract
Yang Chen
Abstract
While Thrust Vector Control used in air to air missile,it increased the maneuver capacity of missile.However,it also take energy consume of the rocket.The effective method of designed missile initial trajectory is discussed by using genetic algorithm,and the best cooperation in ability between maneuver and energy consume is achieved.The model of trajectory optimization is constructed.The algorithm design and numeral simulation is completed.The results are given,and the adaptability,sensibility and efficiency about the algorithm is discussed.
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While Thrust Vector Control used in air to air missile,it increased the maneuver capacity of missile.However,it also take energy consume of the rocket.The effective method of designed missile initial trajectory is discussed by using genetic algorithm,and the best cooperation in ability between maneuver and energy consume is achieved.The model of trajectory optimization is constructed.The algorithm design and numeral simulation is completed.The results are given,and the adaptability,sensibility and efficiency about the algorithm is discussed.
Key concepts: Missile, Air-to-air missile, Trajectory, Genetic algorithm, Range (aeronautics), Engineering, Thrust, Trajectory optimization