Volume 30 Issue 12
Dec.  2015
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LI Zhen-hua, XIAN Yong, LEI Gang, ZHANG Da-qiao, LIU Bing-qi. Rapid optimization design of ascent rendezvous trajectory for launch vehicles based on hybrid particle swarm algorithm[J]. Journal of Aerospace Power, 2015, 30(12): 3029-3034. doi: 10.13224/j.cnki.jasp.2015.12.028
Citation: LI Zhen-hua, XIAN Yong, LEI Gang, ZHANG Da-qiao, LIU Bing-qi. Rapid optimization design of ascent rendezvous trajectory for launch vehicles based on hybrid particle swarm algorithm[J]. Journal of Aerospace Power, 2015, 30(12): 3029-3034. doi: 10.13224/j.cnki.jasp.2015.12.028

Rapid optimization design of ascent rendezvous trajectory for launch vehicles based on hybrid particle swarm algorithm

doi: 10.13224/j.cnki.jasp.2015.12.028
  • Received Date: 2014-04-15
  • Publish Date: 2015-12-28
  • Based on efficiency of gradient search and randomness of particle swarm search, a hybrid particle swarm algorithm was proposed, and applied to research the rapid optimization design of ascent rendezvous trajectory for launch vehicles. Regarding the minimum distance between launch vehicles and target aircraft at intersection point as the objective function, the flight program of solid launch vehicles was designed and an optimization model of ascent rendezvous trajectory was established, and solved by the hybrid particle swarm algorithm, genetic algorithm and particle swarm algorithm. The simulation results indicat that:the algorithm can solve the optimization design problem effectively, the average error of rendezvous position is 4.137m, 17.940m less than genetic algorithm, and the average optimization time is 488.922s, 2342.125s shorter than particle swarm algorithm. The algorithm can be applied to the rapid optimization design of ascent rendezvous trajectory for launch vehicles because of its faster search speed and higher convergence accuracy.

     

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  • [1]
    龙乐豪.总体设计(上)[M].北京:宇航出版社,1989.
    [2]
    雍恩米,陈磊,唐国金.飞行器轨迹优化数值方法综述[J].宇航学报,2008,29(2):397-406. YONG Enmi,CHEN Lei,TANG Guojin.A survey of numerical methods for trajectory optimization of spacecraft[J].Journal of Astronautics,2008,29(2):397-406.(in Chinese)
    [3]
    杨希祥,张为华.基于Gauss伪谱法的固体运载火箭上升段轨迹快速优化研究[J].宇航学报,2011,32(1):15-20. YANG Xixiang,ZHANG Weihua.Rapid optimization of ascent trajectory for solid launch vehicles based on Gauss pseudospectral method[J].Journal of Astronautics,2011,32(1):15-20.(in Chinese)
    [4]
    杨希祥,李晓斌,肖飞,等.智能优化算法及其在飞行器优化设计领域的应用综述[J].宇航学报,2009,30(6):2051-2061. YANG Xixiang,LI Xiaobin,XIAO Fei,et al.Overview of intelligent optimization algorithm and its application in flight vehicles optimization design[J].Journal of Astronautics,2009,30(6):2051-2061.(in Chinese)
    [5]
    罗亚中,唐国金,周黎妮.混合遗传算法及其在运载火箭最优上升轨道设计中的应用[J].国防科学技术大学学报,2004,26(2):5-8. LUO Yazhong,TANG Guojin,ZHOU Lini.Hybrid genetic algorithm and its application to the optimal ascent trajectory design of the vehicle[J].Journal of National University of Defense Technology,2004,26(2):5-8.(in Chinese)
    [6]
    Bessette C R,Spencer D B.Optimal space trajectory design:a heuristic-based approach[R].Tampa,FL:AAS/AIAA Space Flight Mechanics Meeting,2006.
    [7]
    Armellin R,Lavagna M,Starkey R P,et al.Aerogravity-assist maneuvers:coupled trajectory and vehicle shape optimization[J].Journal of Spacecraft and Rockets,2007,44(5):1051-1059.
    [8]
    黄友锐,智能优化算法及其应用[M].北京:国防工业出版社,2008.
    [9]
    Coverstone C V.Near optimal low thrust trajectories optimization via microgenetic algorithms[J].Journal of Guidance,Control and Dynamics,1996,20(1):196-198.
    [10]
    鲜勇,许立军.遗传算法在导弹飞行程序设计中的应用研究[J].系统仿真学报,2009,21(5):1502-1504 XIAN Yong,XU Lijun.Study of designing trajectory missile's flight process based on genetic algorithm[J].Journal of System Simulation,2009,21(5):1502-1504.(in Chinese)
    [11]
    Crain T P,Bishop R H,Fowler W T,et al.Interplanetary flyby mission optimization using a hybrid global/local search method[J].Journal of Spacecraft and Rockets,2000,37(4):468-474.
    [12]
    Qazi M U D,He L,Elhabian T.Rapid trajectory optimization using computational intelligence for guidance and conceptual design of multistage space launch vehicles[R].AlAA 2005-6062,2005.
    [13]
    Al-Garni A,Kassem A H.On the optimization of aerospace plane ascent trajectory[J].Transactions of the Japan Society for Aeronautical and Space Sciences,Space Technology Japan,2007,50(168):113-120.
    [14]
    杨希祥,江振宇,张为华.基于粒子群算法的固体运载火箭上升段弹道优化设计研究[J].宇航学报,2010,31(5):1304-1309. YANG Xixiang,JIANG Zhenyu,ZHANG Weihua.A particle swarm optimization algorithm based solid launch vehicle ascent trajectory optimum design[J].Journal of Astronautics,2010,31(5):1304-1309.(in Chinese)
    [15]
    冉茂鹏,王青.一种基于EPSO的航天器交会轨迹优化方法[J].宇航学报,2013,34(9):1195-1201. RAN Maopeng,WANG Qing.Spacecraft rendezvous trajectory optimization method based on EPSO[J].Journal of Astronautics,2013,34(9):1195-1201.(in Chinese)
    [16]
    孙丕忠,夏智勋,郭振云.水平空中发射固体运载火箭轨道设计与优化[J].固体火箭技术,2004,27(2):87-90. SUN Pizhong,XIA Zhixun,GUO Zhenyun.Trajectory calculation optimization of horizontally air-launched vehicle with wings[J].Journal of Solid Rocket Technology,2004,27(2):87-90.(in Chinese)
    [17]
    张毅,肖龙旭,王顺宏.弹道导弹弹道学[M].长沙:国防科学技术大学出版社,1993.
    [18]
    汪定伟,王俊伟,王洪峰,等.智能优化方法[M].北京:高等教育出版社,2007.
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