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Trajectory Optimization Design for Morphing Wing Missile 被引量:1

Trajectory Optimization Design for Morphing Wing Missile
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摘要 This paper presents a new particle swarm optimization( PSO) algorithm to optimize the trajectory of morphing-wing missile so as to achieve the enlargement of the maximum range. Equations of motion for the twodimensional dynamics are derived by treating the missile as an ideal controllable mass point. An investigation of aerodynamic characteristics of morphing-wing missile with varying geometries is performed. After deducing the optimizing trajectory model for maximizing range,a type of discrete method is put forward for taking optimization control problem into nonlinear dynamic programming problem. The optimal trajectory is solved by using PSO algorithm and penalty function method. The simulation results suggest that morphing-wing missile has the larger range than the fixed-shape missile when launched at supersonic speed,while morphing-wing missile has no obvious range increment than the fixed-shape missile at subsonic speed. This paper presents a new particle swarm optimization( PSO) algorithm to optimize the trajectory of morphing-wing missile so as to achieve the enlargement of the maximum range. Equations of motion for the twodimensional dynamics are derived by treating the missile as an ideal controllable mass point. An investigation of aerodynamic characteristics of morphing-wing missile with varying geometries is performed. After deducing the optimizing trajectory model for maximizing range,a type of discrete method is put forward for taking optimization control problem into nonlinear dynamic programming problem. The optimal trajectory is solved by using PSO algorithm and penalty function method. The simulation results suggest that morphing-wing missile has the larger range than the fixed-shape missile when launched at supersonic speed,while morphing-wing missile has no obvious range increment than the fixed-shape missile at subsonic speed.
出处 《Journal of Harbin Institute of Technology(New Series)》 EI CAS 2015年第5期25-30,共6页 哈尔滨工业大学学报(英文版)
基金 Sponsored by the Natural Science Association Foundation(NSAF)of China(Grant No.11176012) the Research Innovation Project for Graduate Student of Jiangsu-Provincial Ordinary University(Grant No.KLYX15-0394)
关键词 morphing wing missile trajectory optimization optimization model particle swarm optimization(PSO) morphing wing missile trajectory optimization optimization model particle swarm optimization(PSO)
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