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小卫星快速机动与高精度稳定控制分配策略 被引量：1

Control allocation strategy for large angle maneuver and high precision stability control of agile small satellite
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摘要 为满足灵敏小卫星大角度姿态快速机动与机动后快速高精度稳定的需求,针对具有推力器与飞轮等异构执行机构的冗余配置方案,提出了一种在轨动态选择执行机构实施机动任务的控制分配策略.基于优化方法的控制分配算法将期望控制量在冗余混合执行机构间进行动态分配,根据卫星当前状态适时改变优化目标函数中各控制指令的权重,最后通过标准化的求解过程来完成对执行机构的动态选择.最后,针对Microsim仿真平台的执行机构配置所进行的数学仿真结果表明,该策略能够完成小卫星大角度姿态快速机动与高精度稳定的控制分配任务,并满足特定时期选择特定执行机构执行任务,以及限制最大机动角速度等约束条件. To meet the demand of quick maneuver at large angle and high precision stability during the process of maneuver for an agile small satellite,a control allocation strategy is proposed in this paper to control the maneuvering process with configuration of redundant thrusters and reaction wheels.The control allocation algorithm distributes the control requirement among mixed redundant actuators dynamically and changes the weights of control parameters presented in the optimized objective function to choose suitable actuators actuated.The normalized linear programming model is used to obtain the solution.The results of simulation on Microsim platform which is equipped with redundant thrusters and reaction wheels demonstrate the effectiveness of the proposed strategy.
作者 唐生勇 张世杰 陈闽 张育林
机构地区 哈尔滨工业大学卫星技术研究所 国防科技大学航天与材料工程学院
出处 《哈尔滨工业大学学报》 EI CAS CSCD 北大核心 2010年第7期1019-1024,共6页 Journal of Harbin Institute of Technology
基金 国家自然科学基金资助项目(60704020) 长江学者和创新团队发展计划资助项目(IRT0520) 教育部博士点基金(20070213068)
关键词 小卫星 姿态控制 控制分配 大角度机动 高精度稳定 small satellite attitude control control allocation maneuver at large angle high precision sta-bility
分类号 V448.22 [航空宇航科学与技术—飞行器设计]
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参考文献14

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共引文献15

同被引文献15

  • 1燕飞,秦世引.基于RBF神经网络和M距离的卫星故障诊断[J].航天控制,2006,24(6):61-66. 被引量：4
  • 2周树德,孙增圻.分布估计算法综述[J].自动化学报,2007,33(2):113-124. 被引量：209
  • 3唐生勇,张世杰.一种小卫星快速机动与高精度稳定控制分配策略[C]//2008中国空间科学学会空间机电与空间光学专业委员会学术年会论文集.兰州:中国空间科学学会空间机电与空间光学专业委员会,2008:211-216.
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哈尔滨工业大学学报
2010年 第7期

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