航空学报 > 2007, Vol. 28 Issue (5): 1091-1097

航天器复杂约束姿态机动的自主规划

仲维国,崔平远,崔祜涛   

  1. 哈尔滨工业大学 深空探测基础研究中心
  • 收稿日期:2006-10-10 修回日期:2007-05-08 出版日期:2007-10-15 发布日期:2007-10-15
  • 通讯作者: 仲维国

Autonomous Attitude Maneuver Planning for Spacecraft under Complex Constraints

Zhong Weiguo,Cui Pingyuan,Cui Hutao   

  1. Deep Space Exploration Research Center, Harbin Institute of Technology
  • Received:2006-10-10 Revised:2007-05-08 Online:2007-10-15 Published:2007-10-15
  • Contact: Zhong Weiguo

摘要:

研究了星载设备经受动态环境的多种几何约束和动力学约束时,航天器姿态机动历程的星上规划方法。将完整姿态映射为三维姿态描述空间中的点,姿态路径的规划问题转化为中间节点的规划。随机搜索空间中的一组节点,在相邻节点间采用施加动力学约束的Euler转动姿态制导律,并考查Euler转动过程中的几何约束。用快速搜索随机树方法搜索到可行解,再利用姿态空间特性对路径加以优化。仿真显示算法能在大范围内快速得到可行解,优化措施有助缩短机动时间。离散化的节点规划保证了复杂约束情况下解的有效性,并具有概率完备性。

关键词: 飞行器控制, 路径规划, 随机搜索, 运动优化, 姿态机动

Abstract:

For spacecraft suffering from multiple celestial constraints in timevarying space environment, along with intrinsic dynamics constraints, an onboard attitude maneuver planning was studied. The full attitude was mapped to a point described in threedimensional attitude space. The attitude path planning was then transformed to sequent plannings of intermediate nodes. A set of nodes were randomly searched in the attitude space.

Key words: spacecraft , control,  , path , planning,  , random , search,  , motion , optimization,  , attitude , maneuver

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