期刊文献+

基于三分图的非共面卫星分布式加注任务规划 被引量:2

Mission Programming of Peer-to-Peer Refueling on Non-Coplanar Circular Orbit
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摘要 分布式加注规划的目的在于规划加注过程的交会路径,使任务在满足约束的情况下整体燃料消耗最优。针对异面圆轨道卫星间的分布式加注策略,建立了分布式加注任务规划问题的数学模型,把该规划问题归结为非完全赋权三分图的匹配问题,并将整体最少燃料消耗作为规划目标。其次,进行了算法的流程设计,采用了Kuhn-Mundres图论算法和整数遗传算法相结合的LSGA算法加快了收敛的速度保证了全局最优。最后,选取了两个具有小角度轨道偏差的异面卫星星座对该问题进行分析。计算得到了优化后的双冲量机动下加注任务的服务关系与燃料代价,规划算法的有效性也得到了验证。 The aim of the optimal schedule for the Peer-to-Peer refueling strategy is to find the best rendezvous trajectories with the minimum fuel consumption during the whole mission. Firstly, the mathematic model for the mission programming was set up, which was summed up as a three-index match problem, and the minimum fuel expenditure was set to be the objective. Secondly, the algorithm flow for the problem was designed, and the combination of Kuhn-Mundres algorithm and the integer genetic algorithm were adopted, the convergence was accelerated and the global optimization was guaranteed. At last, two constellations in the non-coplanar circular orbit with a small intersection angle was considered as an example, and the optimal scheduling and fuel cost for two impulse maneuver were gotten successfully. And the result shows that the proposed model and algorithm are efficient.
出处 《中国空间科学技术》 EI CSCD 北大核心 2015年第1期58-65,共8页 Chinese Space Science and Technology
基金 国家自然科学基金(51205403) 863基金(2013AA7045040 2013AA7044029)资助项目
关键词 在轨加注 三分图 整数遗传算法 任务规划 异面圆轨道 卫星 On-orbit refueling Tripartite graph Integer genetic algorithm Mission programming Non-coplanar circular orbit Satellite
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参考文献8

  • 1HEATON A F, HOWARD R T, PINSON R M. Orbital Express AVGS validation and calibration forautomated rendezvous [C]. AIAA/AAS Astrodynamics Specialist Conference and Exhibition,Honolulu,Hawaii, 2008.
  • 2欧阳琦,姚雯,陈小前.地球同步轨道卫星群在轨加注任务规划[J].宇航学报,2010,31(12):2629-2634. 被引量:24
  • 3DUTTA A,TSIOTRAS P. Asynchronous optimal mixed P2P satellite refueling strategies [J]. TheJournal of Astronautical Sciences,2006,54(3-4) : 543-565.
  • 4DUTTA A, TSIOTRAS P. Network flow formulation for cooperative peer-to-peer refueling strategies [J].Journal Of Guidance Control and Dynamics,2010, 33(5) : 1539-1549.
  • 5DUTTA A. Optimal cooperative and non-cooperative peer-to-peer maneuvers for refueling satellites in circularconstellations [D]. Atlanta: Georgia Institute of Technology,2009.
  • 6ALFRIEND K T,LEE D? CREAMER N G. Optimal servicing of geosynchronous satellites [J]. Journalof Guidance Control and Dynamics, 2006,29(1) : 203-206.
  • 7韩潮,谢华伟.空间交会中多圈Lambert变轨算法研究[J].中国空间科学技术,2004,24(5):9-14. 被引量:32
  • 8HUANG G, LIM A. A hybrid genetic algorithm for the three-index assignment problem [J]. EuropeanJournal of Operational Research, 2006,172(1) : 249-257.

二级参考文献4

  • 1[3]肖业伦. 航天器飞行动力学原理. 北京:宇航出版社,1995.
  • 2Tsiotras P,Nailly A.Comparison between peer-to-peer and single spacecraft refueling strategies for spacecraft in circular orbits[R].AIAA 2005-7115.AIAA.2005.
  • 3Kyle T,Deok-Jin Lee,Glenn Creamer N.Optimal servicing of geosynchronous satellites[R].AIAA 2002-4905.AIAA.2002.
  • 4韩潮,段彬,付红勋.远程导引可行飞行方案寻求算法研究[J].中国空间科学技术,2002,22(1):47-52. 被引量:10

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