期刊文献+

基于APSO的微纳卫星编队轨迹规划方法

APSO-based Trajectory Planning Method for Micro-nano Satellite Formation
下载PDF
导出
摘要 针对微纳卫星编队在指定时间内由初始构型到指定构型的路径规划问题,提出了一种基于自适应惯性权重粒子群优化(adaptive-inertial-weightedparticleswarmoptimization,APSO)算法的轨迹规划方法。首先,通过Radau伪谱法将轨迹规划的连续最优控制问题离散化为参数优化的非线性规划(nonlinear programming, NLP)问题;其次,采用APSO算法对NLP问题求解,避免了复杂梯度求解困难的问题,同时降低了计算量;最后,通过仿真实验表明,所提方法可在更短时间内求得满足约束条件的最优轨迹,以完成在线轨迹规划任务。 To deal with the path planning problem of micro nano satellite formation from initial configuration to specified configuration in a specified time,a trajectory planning method based on adaptive inertial weighted particle swarm optimization(APSO)is proposed.Firstly,the continuous optimal trajectory planning problem is transformed into the NLP problem of parameter optimization by using Radau pseudospectral method.Secondly,the APSO algorithm is used to solve the NLP problem,the gradient solution is avoided and the cost of computation is reduced.Finally,the simulation indicates that this method can get the optimal trajectory,which takes less time and meets the needs of online trajectory planning.
作者 刘金魁 郭健 周川 吴益飞 韩飞 LIU Jinkui;GUO Jian;ZHOU Chuan;WU Yifei;HAN Fei(School of Automation,Nanjing University of Science and Technology,Nanjing 210094,China;Shanghai Key Laboratory of Aerospace Intelligent Control Technology,Shanghai Institute of Spaceflight Control Technology,Shanghai 201109,China)
出处 《控制工程》 CSCD 北大核心 2024年第3期457-462,共6页 Control Engineering of China
基金 国家重点研发计划资助项目(2016YFB0501003) 教育部科技发展中心产学研创新基金资助项目(2020QT06)。
关键词 卫星编队 轨迹规划 Radau伪谱法 APSO Satellite formation trajectory planning Radau pseudospectral method APSO
  • 相关文献

参考文献3

二级参考文献31

  • 1吴昊,刘建业,段方,赵伟.基于STK的小卫星轨道交会设计研究[J].飞行器测控学报,2005,24(2):40-44. 被引量:3
  • 2张雅声 ,张育林 .性能修复型星座快速重构方法研究[J].装备指挥技术学院学报,2005,16(4):66-72. 被引量:10
  • 3Acikmese A B, Schar D P, Murray E A, et al. A convex guidance algorithm for formation reconfiguration [C] // AIAA Guidance, Navigation, and Control Conference and Exhibit. Reston, USA: AIAA, 2006: 1-17.
  • 4Scharf D P, Hadaegh F Y, P!.oen S R. A survey of space craft formation flying guidance and control (Part I): guidance [C] // Proceedings of the American Control Conference. Denver, USA: American Automatic Control Council, 2003, 1733 1739.
  • 5Singh G, Hadaegh F Y. Collision avoidance guidance for formation-flying applications[C]//AIAA Guidance Navi gation, and Control Conference and Exhibition. Reston, USA~ AIAA, 2001:1 11.
  • 6Sultan C, Seereram S, Mehra R K. Deep space formation flying spacecraft path planning[J].The International Journal of Robotics Research, 2007, 26(4):405-430.
  • 7Richards A, Schouwenaars T, How J P, et al. Spacecraft trajectory planning with avoidance constraints using mixed-integer linear programming[J]. Journal of Guidance, Control, and Dynamics, 2002, 25(4): 755-764.
  • 8Cetin B, Bikdash M, Hadaegh F Y. Hybrid mixed-logical linear programming algorithm for collision free optimal path planning[J]. lET Control Theory ~ Applications, 2007, 1(2): 522-531.
  • 9Garcia I, How J P. Trajectory optimization for satellite reconfiguration maneuvers with position and attitude con straints[C]//Proceedings of the American Control Confer- Portland, USA:American Automatic Control Council, 2005, 2:889-894.
  • 10Aoude G S, How J P, Gareia I M. Two-stage path plan ning approach for designing multiple spacecraft reconfigu ration maneuvers[C] // Proceedings of the 20th Interna tional Symposium on Space Flight Dynamics. Piscataway USA: IEEE, 2007.

共引文献17

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部