Disturbance Observer-Based Attitude Control for Spacecraft With Input MRS

Zou An-Min; de Ruiter Anton H. J.; Kumar Krishna Dev

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Disturbance Observer-Based Attitude Control for Spacecraft With Input MRS

机译：具有输入MRS的航天器基于干扰观测器的姿态控制

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This paper considers the problem of attitude tracking control for uncertain rigid spacecraft subject to control input magnitude and rate saturation (MRS). First, a smooth input MRS model is proposed. Then, a robust attitude tracking control scheme is designed based on the backstepping and finite-time disturbance observer techniques. Finally, the effectiveness of the control scheme derived here is illustrated by numerical simulations.

机译：本文考虑了受输入大小和速率饱和度（MRS）控制的不确定刚性航天器的姿态跟踪控制问题。首先，提出了一种平滑的输入MRS模型。然后，基于反推和有限时间干扰观测器技术，设计了一种鲁棒的姿态跟踪控制方案。最后，通过数值仿真说明了此处导出的控制方案的有效性。

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《IEEE Transactions on Aerospace and Electronic Systems》 |2019年第1期|384-396|共13页
作者
Zou An-Min; de Ruiter Anton H. J.; Kumar Krishna Dev;
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Shantou Univ, Coll Engn, Dept Elect Engn, Shantou 515063, Peoples R China|Ryerson Univ, Dept Aerosp Engn, Toronto, ON M5B 2K3, Canada;

Ryerson Univ, Dept Aerosp Engn, Toronto, ON M5B 2K3, Canada;

Ryerson Univ, Dept Aerosp Engn, Toronto, ON M5B 2K3, Canada;

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1. Disturbance observer-based attitude stabilization for rigid spacecraft with input MRCs [J] . Keke Shi, Chuang Liu, Zhaowei Sun, Advances in space research . 2020,第3期

机译：基于干扰的抗干扰观察者态度稳定，刚性航天器与输入MRCS
2. Extended harmonic disturbance observer-based attitude control for flexible spacecraft with control moment gyroscopes [J] . Huang Liya, Wu Zhong Proceedings of the Institution of Mechanical Engineers . 2019,第14期

机译：带有控制力矩陀螺仪的挠性航天器基于扩展谐波干扰观测器的姿态控制
3. Disturbance observer-based fault-tolerant attitude tracking control for rigid spacecraft with finite-time convergence [J] . Zong Qun, Zhang Xiuyun, Shao Shikai, Proceedings of the Institution of Mechanical Engineers . 2019,第2期

机译：基于扰动观测器的有限时间刚性航天器容错姿态跟踪控制
4. Disturbance observer-based attitude control of spacecraft with single-gimbal control moment gyros [C] . Ruidong Yan, Wu Zhong World Congress on Intelligent Control and Automation . 2014

机译：单扰动控制陀螺仪的基于干扰观测器的航天器姿态控制
5. Spacecraft Attitude Control Program: A spacecraft attitude determination and control simulation program. [D] . Rajagopalan, Murlidhar. 1996

机译：航天器姿态控制程序：航天器姿态确定和控制模拟程序。
6. Finite-Time Attitude Stabilization Adaptive Control for Spacecraft with Actuator Dynamics [O] . Chunbao Wang, Dong Ye, Zhongcheng Mu, 2019

机译：具有执行器动力学的航天器航天器的有限时间态度稳定控制
7. Anti-disturbance inverse optimal control for spacecraft position and attitude maneuvers with input saturation [O] . Chutiphon Pukdeboon 2016

机译：具有输入饱和的航天器位置和姿态机动的抗干扰逆最优控制

Disturbance Observer-Based Attitude Control for Spacecraft With Input MRS

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