基于广义逆的欠驱动航天器姿态机动控制

黄静; 李传江; 马广富; 刘刚

doi:10.3724/SP.J.1004.2013.00285

基于广义逆的欠驱动航天器姿态机动控制

doi: 10.3724/SP.J.1004.2013.00285

1.
哈尔滨工业大学控制科学与工程系哈尔滨 150001

详细信息

通讯作者:
黄静

计量
- 文章访问数: 1986
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- 被引次数: 0
出版历程
- 收稿日期: 2011-01-17
- 修回日期: 2012-07-25
- 刊出日期: 2013-03-20

Generalised Inversion Based Maneuver Attitude Control for Underactuated Spacecraft

1.
Department of Control Science and Engineering, Harbin Institute of Technology, Harbin 150001

摘要

摘要: 针对欠驱动刚体航天器机动控制问题,应用广义逆方法设计了姿态机动控制器. 首先将三轴稳定欠驱动航天器动力学和运动学系统分解为三个子系统, 应用微分几何理论将欠驱动航天器子系统转化为逐点线性形式, 并设计了欠驱动航天器子系统渐近稳定控制器,进一步引入了动态尺度广义逆和摄动零控制向量, 实现了对另外两轴的控制.设计的广义逆姿态控制器保证了整个系统的渐近稳定性, 达到了控制要求. 数值仿真实验结果表明了所设计控制律的有效性.
- 航天器 /
- 欠驱动系统 /
- 姿态机动 /
- 广义逆方法
Abstract: The methodology based on the concept of generalized inversion is investigated for asymptotic stabilization of underactuated rigid body dynamics under two degrees of actuation. Firstly, the underactuated kinematics and dynamics system is partitioned into three subsystems, and the underactuated subsystem is transformed as the point-wise linear form by differential geometry theory and achieves global realisability. Furthermore, with the introduction of dynamically scaled generalized inversion and perturbed null-control vector, a continuous feedback control law is designed to achieve the attitude stabilization of the underactuated spacecraft. Finally, the analytical and simulation results show that the proposed control methodology is effective.
- Spacecraft /
- underactuated system /
- attitude maneuver /
- generalised inverse method

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参考文献(1)

[1]

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