Modeling and control of a flexible spacecraft for large-angel rapid maneuvers

机译：用于大角度快速机动的挠性航天器的建模和控制

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This paper deals with large-angle rapid slew maneuvers of a flexible spacecaft, which consists of a rigid central body and a flexible beam attached to it. Dynamic model for the spacecraft described by a coupled noninear bybrid system is derived. With the control torque applied to the rigid central body only, a PD control law is presented using the measurements of the attitude angle of the rigid body and its velocity. based upon the Lyapunov method in infinite dimensional space, it is shown that implementation of the control algorithm results in the slew maneuvering with the simultaneous vibration suppression.

机译：本文研究了挠性太空船的大角度快速回转操作，该飞船由刚性的中心体和与其相连的柔性梁组成。推导了由耦合的非近旁混合系统描述的航天器动力学模型。在仅将控制转矩施加到刚性中心体的情况下，使用对刚性体的姿态角及其速度的测量结果，得出PD控制律。基于Lyapunov方法在无穷维空间中的控制结果表明，控制算法的实现导致回转操纵同时抑制振动。

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来源
《4th IFAC(International Federation of Automatic Control) Symposium on Automatic Control in Aerospace 1998 Seoul, Korea, 24-28 August 1998》|1998年|p.341-346|共6页
会议地点 Seoul(KR)
作者
Yong Li;
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原文格式 PDF
正文语种 eng
中图分类航空、航天技术的研究与探索;
关键词
structure systems; nonlinear models; distributed-parameter systems; PD contrllers; stability analysis.;

机译：结构系统；非线性模型分布参数系统； PD控制器；稳定性分析。;

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1. Nonlinear dynamic modeling and decoupling for rigid-flexible coupled system of spacecraft with rapid maneuver [J] . Cao Yuteng, Cao Dengqing, Huang Wenhu Proceedings of the Institution of Mechanical Engineers, Part C. Journal of mechanical engineering science . 2019,第14期

机译：快速动作刚性柔性耦合系统的非线性动态建模与去耦
2. Reference Model Variable Structure Output Feedback For Attitude Maneuvers Control Of Flexible Spacecrafts [J] . QINGLEI HU, XIAO-ZHI GAO, GUANGFU MA Intelligent automation and soft computing . 2009,第1期

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3. Inverse Dynamics based Model Predictive Control for Spacecraft Rapid Attitude Maneuver [J] . Chao Song, Genaro Islas, Klaus Schilling IFAC PapersOnLine . 2019,第12期

机译：基于逆动力学的航天器快速姿态机动模型预测控制
4. Modeling and control of a flexible spacecraft for large-angel rapid maneuvers [C] . Yong Li International Federation of Automatic Control symposium on automatic control in aerospace . 1999

机译：柔性宇宙飞船对大天使快速演习的建模与控制
5. Modeling and slew-maneuver control of a flexible spacecraft. [D] . Eckhart, Jeremy E. 2005

机译：挠性航天器的建模和回转操纵控制。
6. Deep Generative Models-Based Anomaly Detection for Spacecraft Control Systems [O] . Hyojung Ahn, Dawoon Jung, Han-Lim Choi 2020

机译：基于深度生成模型的航天器控制系统异常检测
7. Fast Attitude Maneuver of a Flexible Spacecraft with Passive Vibration Control Using Shunted Piezoelectric Transducers [O] . Bassam A. Albassam 2019

机译：使用分流压电传感器的无源振动控制快速姿态机动
8. Optimization of Closed Loop Eigenvalues: Maneuvering, Vibration Control, and Structure/Control Design Iteration for Flexible Spacecraft [R] . Junkins, J. L. 1986

机译：闭环特征值的优化：柔性航天器的机动，振动控制和结构/控制设计迭代

Modeling and control of a flexible spacecraft for large-angel rapid maneuvers

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