引用本文: | 赵波林,刘昆,张立.控制力矩陀螺的动态扫描成像卫星姿态控制.[J].国防科技大学学报,2016,38(4):119-124.[点击复制] |
ZHAO Bolin,LIU Kun,ZHANG Li.Attitude control of dynamic scanning imaging satellite of control moment gyros[J].Journal of National University of Defense Technology,2016,38(4):119-124[点击复制] |
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控制力矩陀螺的动态扫描成像卫星姿态控制 |
赵波林, 刘昆, 张立 |
(国防科技大学 航天科学与工程学院, 湖南 长沙 410073)
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摘要: |
针对卫星动态扫描成像任务中的姿态控制问题,建立卫星姿态动力学模型,分析动态扫描成像任务对姿态控制的特殊需求。结合动态扫描成像任务需求提出一种典型的姿态机动方案,对姿态机动过程所需控制力矩进行估计。基于期望力矩和星体实时姿态设计一种俯仰机动控制律,并提出五棱锥构型陀螺群的操纵方案。针对某动态扫描成像任务卫星,对提出的控制律进行数值仿真。仿真结果证明所提方案可以满足卫星动态扫描成像的姿态控制要求。 |
关键词: 动态扫描成像 姿态控制 姿态机动方案 俯仰机动控制律 五棱锥构型陀螺群 |
DOI:10.11887/j.cn.201604019 |
投稿日期:2015-04-27 |
基金项目:国家自然科学基金青年科学基金资助项目(61503395) |
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Attitude control of dynamic scanning imaging satellite of control moment gyros |
ZHAO Bolin, LIU Kun, ZHANG Li |
(College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China)
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Abstract: |
According to the problem of attitude control of satellite dynamic scanning imaging, the dynamic model of the satellite attitude was built and the specific requirement of dynamic scanning imaging tasks for attitude control was analyzed. Combined with the dynamic scanning imaging tasks, a typically attitude maneuver scheme was designed. The required control moment of the process of dynamic scanning imaging was estimated. A pitching maneuver control law based on the expected torque and real-time attitude of satellite was developed, and the steering law of five pyramid configuration gyros was given. A numerical simulation was presented for the designed control law based on a maneuver task. The simulation results proved that the proposed scheme can satisfy the requirement of attitude control of dynamic scanning imaging satellite. |
Keywords: dynamic scanning imaging attitude control attitude maneuver scheme pitching maneuver control law five pyramid configuration gyros |
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