[1]吴利平,郭 毓,姚 伟,等.一种太阳帆航天器姿态机动控制方法[J].南京理工大学学报(自然科学版),2016,40(03):272.[doi:10.14177/j.cnki.32-1397n.2016.40.03.004]
 Wu Liping,Guo Yu,Yao Wei,et al.Attitude maneuver control method for solar sail[J].Journal of Nanjing University of Science and Technology,2016,40(03):272.[doi:10.14177/j.cnki.32-1397n.2016.40.03.004]
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一种太阳帆航天器姿态机动控制方法
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《南京理工大学学报》(自然科学版)[ISSN:1005-9830/CN:32-1397/N]

卷:
40卷
期数:
2016年03期
页码:
272
栏目:
出版日期:
2016-06-30

文章信息/Info

Title:
Attitude maneuver control method for solar sail
文章编号:
1005-9830(2016)03-0272-06
作者:
吴利平郭 毓姚 伟郭 健
南京理工大学 自动化学院,江苏 南京 210094
Author(s):
Wu LipingGuo YuYao WeiGuo Jian
School of Automation,Nanjing University of Science and Technology,Nanjing 210094,China
关键词:
太阳帆 姿态控制 控制杆 俯仰轴 刚柔耦合模型 挠性模态 反馈控制 比例 积分 状态误差
Keywords:
solar sails attitude control gimbal boom pitch axis rigid-flexible coupling model flexible modes feedback control proportion integral state error
分类号:
TP273; V448.22
DOI:
10.14177/j.cnki.32-1397n.2016.40.03.004
摘要:
针对太阳帆航天器挠性模态易激发但难测量的问题,该文研究以控制杆作为执行机构的太阳帆航天器姿态控制。基于控制杆的动力学分析建立了太阳帆俯仰轴刚柔耦合模型。提出了1种姿态机动路径柔化与可测刚体姿态信息反馈控制相结合的太阳帆姿态控制方法。设计了比例积分型状态误差反馈律,并给出了使系统刚体姿态与挠性模态均渐近稳定的充分条件。仿真结果表明,所提控制方法能较好地满足太阳帆姿态调整的快速性与准确性要求。
Abstract:
Due to the problem of solar sails that it is easy to excite but difficult to detect the flexible modes,an attitude control method for a solar sail is studied using a gimbal boom as the actuator.A rigid-flexible coupling model for the pitch axis is established with the dynamics of the gimbal boom.A novel attitude control method is proposed combining a path planning method with a measurable-rigid-information feedback controller.A proportion-integral(PI)state error feedback control law is designed,and an asymptotical stabilization condition for both rigid states and flexible modes is given.The numerical simulation results demonstrate the proposed control method can satisfy the rapidity and accuracy of attitude adjustment for solar sails.

参考文献/References:

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备注/Memo

备注/Memo:
收稿日期:2015-09-17 修回日期:2015-12-14
基金项目:国家自然科学基金(61473152)
作者简介:吴利平(1990-),女,博士生,主要研究方向:太阳帆航天器姿态控制,E-mail:wulp0724@163.com; 通讯作者:郭毓(1964-),女,博士,教授,主要研究方向:挠性航天器姿态控制、高精度伺服系统、机器人技术等,E-mail:guoyu@njust.edu.cn。
引文格式:吴利平,郭毓,姚伟,等.一种太阳帆航天器姿态机动控制方法[J].南京理工大学学报,2016,40(3):272-277.
投稿网址:http://zrxuebao.njust.edu.cn
更新日期/Last Update: 2016-06-30