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交会对接远程导引轨道控制状态规划与优化算法
引用本文:伍升钢,侯黎强,张智斌,谭炜,李恒年.交会对接远程导引轨道控制状态规划与优化算法[J].飞行器测控学报,2012(4):90-94.
作者姓名:伍升钢  侯黎强  张智斌  谭炜  李恒年
作者单位:宇航动力学国家重点实验室;中国西安卫星测控中心
摘    要:对空间交会对接远程导引段轨道控制问题进行了研究。在简单介绍交会对接远程导引轨道控制实时规划模型的基础上,提出了基于近圆偏差方程、序列二次规划算法和目标权重函数等在不同控制目标模式下的状态规划与优化算法。仿真结果表明,该算法收敛速度快,能较好地满足交会对接远程导引段的轨道控制要求,具有一定的工程实用价值。

关 键 词:交会对接  远程导引段  近圆偏差方程  序列二次规划算法  轨道控制

Planning and Optimization Algorithms of Phasing Orbit Manoeuvres in Rendezvous and Docking
WU Shenggang,HOU Liqiang,ZHANG Zhibin,TAN Wei,LI Hengnian.Planning and Optimization Algorithms of Phasing Orbit Manoeuvres in Rendezvous and Docking[J].Journal of Spacecraft TT&C Technology,2012(4):90-94.
Authors:WU Shenggang  HOU Liqiang  ZHANG Zhibin  TAN Wei  LI Hengnian
Institution:1(1.State Key Laboratory of Astronautic Dynamics,Xi’an 710043;2.Xi’an Satellite Control Center,Xi’an 710043)
Abstract:Phasing of orbit maneuvers in space rendezvous and docking in the remote guidance phase is studied.Following a brief introduction of the real-time planning model for phasing of orbit maneuvers in space rendezvous and docking,state planning and optimization algorithms in different modes based on near-circular deviation equations,sequential quadratic programming and target weighting function are proposed.Simulation results show that the algorithms converge quickly and well meet the requirements of phasing of orbit maneuvers in the remote guidance phase.
Keywords:rendezvous and docking  remote guidance phase  near-circular deviation equations  sequential quadratic programming  orbit maneuvers
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