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航天器近距离导引轨迹规划仿真系统设计

刘涛 赵育善 师鹏 李保军

刘涛, 赵育善, 师鹏, 等 . 航天器近距离导引轨迹规划仿真系统设计[J]. 北京航空航天大学学报, 2012, (4): 513-518.
引用本文: 刘涛, 赵育善, 师鹏, 等 . 航天器近距离导引轨迹规划仿真系统设计[J]. 北京航空航天大学学报, 2012, (4): 513-518.
Liu Tao, Zhao Yushan, Shi Peng, et al. Combined simulation system design for trajectory planning of spacecraft proximity guidance[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, (4): 513-518. (in Chinese)
Citation: Liu Tao, Zhao Yushan, Shi Peng, et al. Combined simulation system design for trajectory planning of spacecraft proximity guidance[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, (4): 513-518. (in Chinese)

航天器近距离导引轨迹规划仿真系统设计

详细信息
  • 中图分类号: TP 391.9

Combined simulation system design for trajectory planning of spacecraft proximity guidance

  • 摘要: 以航天器近距离导引轨迹规划仿真验证为目标,对基于Visual C+ +,Vega Prime和Matlab的联合仿真系统进行开发研究.首先,建立了数学模型.然后,利用Matlab对所建立的数学模型进行优化求解,得到追踪航天器近距离机动时的位置、速度等信息.并通过Multigen Creator软件建立卫星等对象的模型,使用Vega Prime进行视景仿真.之后,采用Visual C+ +进行系统集成,建立基于三者相结合的仿真验证系统.最后,以椭圆参考轨道下近距离交会的连续推力式燃料最优轨迹规划为例,验证了该联合仿真系统.

     

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出版历程
  • 收稿日期:  2010-12-23
  • 刊出日期:  2012-04-30

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