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电磁航天器编队动力学建模与运动规划方法

邵龙飞 师鹏 赵育善

邵龙飞, 师鹏, 赵育善等 . 电磁航天器编队动力学建模与运动规划方法[J]. 北京航空航天大学学报, 2015, 41(4): 737-743. doi: 10.13700/j.bh.1001-5965.2014.0305
引用本文: 邵龙飞, 师鹏, 赵育善等 . 电磁航天器编队动力学建模与运动规划方法[J]. 北京航空航天大学学报, 2015, 41(4): 737-743. doi: 10.13700/j.bh.1001-5965.2014.0305
SHAO Longfei, SHI Peng, ZHAO Yushanet al. Dynamics modeling and motion programming for electromagnetic formation flight[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(4): 737-743. doi: 10.13700/j.bh.1001-5965.2014.0305(in Chinese)
Citation: SHAO Longfei, SHI Peng, ZHAO Yushanet al. Dynamics modeling and motion programming for electromagnetic formation flight[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(4): 737-743. doi: 10.13700/j.bh.1001-5965.2014.0305(in Chinese)

电磁航天器编队动力学建模与运动规划方法

doi: 10.13700/j.bh.1001-5965.2014.0305
基金项目: 国家自然科学基金资助项目(11102007); 中央高校基本科研业务费资助项目(YWF-14-YHXY-012)
详细信息
    作者简介:

    邵龙飞(1989—),男,陕西汉中人,硕士生,shaolongfei@sina.cn

    通讯作者:

    师鹏(1981—),男,陕西咸阳人,讲师,shipeng@buaa.edu.cn,主要研究方向为航天器动力学与控制.

  • 中图分类号: V412.4

Dynamics modeling and motion programming for electromagnetic formation flight

  • 摘要: 基于电磁航天器作用原理,利用拉格朗日方法,建立电磁航天器“绳系”动力学模型.基于偏差线性化动力学模型,以切向、径向编队为例,分析编队构型保持稳定性,设计构型保持控制律;将双星电磁航天器编队(EMFF,Electromagnetic Formation Flight)重构运动规划问题转化为标准优化问题,利用高斯伪谱优化方法进行求解.并提出序列控制策略,将该双星模型扩展应用于多星电磁编队构型重构问题,转化为多阶段运动规划问题利用多阶段优化方法进行求解.仿真结果表明本文的动力学建模方法和控制方法是可行的.

     

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出版历程
  • 收稿日期:  2014-05-28
  • 修回日期:  2014-09-01
  • 刊出日期:  2015-04-20

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