期刊文献+

空间交会调相综合变轨优化 被引量:1

Optimization of Rendezvous Phasing Strategy with Hybrid Maneuvers
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摘要 基于近圆轨道偏差线性方程研究了摄动交会调相综合变轨问题,建立了综合变轨两层非线性优化模型:上层问题以变轨点纬度幅角为优化变量,下层问题以脉冲向量为优化变量。为了快速获得上层问题全局优化性较好的摄动解,采用了并行模拟退火算法与序列二次规划算法相结合的混合策略;下层问题使用基于可行域最速下降的线性迭代方法求解。采用一个两天近地轨道调相问题测试了本文的综合变轨求解策略,并将综合变轨与特殊点变轨、综合变轨混合优化与遗传算法优化进行了比较。结果表明,建立的两层优化模型是有效的,本文的求解策略有着良好的全局收敛性和较高的收敛效率,综合变轨相对于特殊点变轨可以显著地节省燃料。 Based on linear deviation equations on approximate circular orbits, a perturbed rendezvous phasing strategy with hybrid maneuvers is studied. A bi-level nonlinear optimization model is formulated for optimizing this phasing strategy. The higher-level problem is proposed to optimize the argument of latitude at the maneuver location. For rapidly obtaining a better global optimal perturbed solution, a hybrid approach combining parallel simulated annealing algorithm and sequential quadratic programming algorithm is employed. The lower-level problem is to optimize impulse vector, and is solved using linear iteration method, which is based on feasible steepest descent algorithm. The proposed approach is evaluated in a practical twoday rendezvous phasing mission. The comparisons between hybrid maneuvers and special-point maneuvers and also between hybrid maneuvers solved by hybrid approach and by genetic algorithm are made. It is shown that the bi-level nonlinear optimization model is effective, and the hybrid approach has good global convergence ability and high-level convergence efficiency. Compared with special-point maneuvers, hybrid maneuvers can save fuel cost markedly.
出处 《航天控制》 CSCD 北大核心 2009年第1期15-19,24,共6页 Aerospace Control
关键词 空间交会 调相 综合变轨 优化 Rendezvous Phasing Hybrid maneuvers Optimization
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参考文献8

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共引文献123

同被引文献19

  • 1朱仁璋,汤溢,李颐黎,林彦.航天器交会飞行设计方法研究[J].中国空间科学技术,2006,26(1):9-16. 被引量:5
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  • 3贺颖骏.俄“快速对接”发射载人飞船,明年初或彻底过渡到新发射模式[N].新华每日电讯,2013-3-30(3).
  • 4张晓东.俄“联盟”号载人飞船首次与国际空间站快速对接[N].人民日报,2013-3-30(3).
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  • 8Pete Harding.Progress M-16M Successfully Tests New Fast Rendezvous with ISS[EB/OL].[2012-08-01].http://www.nasaspaceflight.com/2012/08/progress-m-16m- launch-test-new-fast-rendezvous-iss.htm.
  • 9宋征宇.从准确、精确到精益求精—载人航天推动运载火箭制导方法的发展[J].航天控制,2013,31(1):4-10.
  • 10李九人,李海阳,蒋自成.空间救援发射窗口分析[J].国防科技大学学报,2008,30(1):10-14. 被引量:8

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