石油化工高等学校学报

石油化工高等学校学报 ›› 2007, Vol. 20 ›› Issue (3): 37-40.

• 优化控制 • 上一篇    下一篇

高超声速飞行器单周期飞行轨迹优化研究

吴迪1 ,2 , 胡鹏1 , 林笑旭1 , 姚宗信1   

  1. 1 .大连理工大学电信学院计算机系, 辽宁大连116024 ;
    2 .沈阳飞机设计研究所, 辽宁沈阳110035
  • 收稿日期:2007-02-05 出版日期:2007-09-20 发布日期:2017-07-05
  • 作者简介:吴迪(1972 -), 男, 辽宁大连市, 副教授, 博士后
  • 基金资助:
    国家863 计划资助项目(2005AA726025)

Optimizatio n on a Period of Flying Orbi t o f Hypersonic Vehicle

  1. 1. Department of Computer Science and Technology, Dalian University of Technology, Dalian Liaoning 116024, P.R. China;  
    2. Shenyang Aircraft Design & Research Institute, Shenyang Liaoning 110035, P.R. China
  • Received:2007-02-05 Published:2007-09-20 Online:2017-07-05
  • Supported by:
    Hypersonic vehicle|    PSO algorithm|    Flying orbit|    Optimization 

摘要: 高超声速飞行器的初始质量和起始角度的大小对飞行器的飞行轨迹有较大影响, 也影响飞行器的其
它参数设计。针对飞行器的飞行情况将飞行轨迹划分为6 个状态, 并建立3 个模型进行分析, 然后使用改进的粒子
群算法, 分别对初始质量、起始角度和水平位移的关系进行了测试, 并参照测试结果对飞行轨迹进行了整体优化研
究。最后通过算例进行了测试和分析, 验证了该方法的合理性和有效性。

关键词: 高超声速飞行器 , 粒子群算法 , 飞行轨迹 , 优化

Abstract:

The magnitude of the original quality and original angle of hypersonic vehicle can influence flying orbit and other design-parameters greatly. Firstly, according to flying process, the flying orbit was divided into six states analyzed by three models. Then a modified particle swarm optimization (PSO) algorithm was used to test the relationship among original quality, original angle and level distance. Referring to the test result, optimization research on a period of flying orbit of hypersonic vehicle was performed. Finally, the method has been successfully used and validated its rationality and validity by testing and analyzing the example.

引用本文

吴迪, 胡鹏, 林笑旭, 姚宗信. 高超声速飞行器单周期飞行轨迹优化研究[J]. 石油化工高等学校学报, 2007, 20(3): 37-40.

WU Di, HU Peng, LIN Xiao-xu, YAO Zong-xin. Optimizatio n on a Period of Flying Orbi t o f Hypersonic Vehicle[J]. Journal of Petrochemical Universities, 2007, 20(3): 37-40.

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