Finite-time output feedback attitude coordination control for formation flying spacecraft without unwinding

Guo Yong; Song Shen-Min; Li Xue-Hui

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Finite-time output feedback attitude coordination control for formation flying spacecraft without unwinding

机译：编队飞行航天器不放卷的有限时间输出反馈姿态协调控制

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In this paper, two finite-time attitude coordinated controllers for formation flying spacecraft are investigated based on rotation matrix. Because rotation matrix can represent the set of attitudes both globally and uniquely, the two controllers can deal with unwinding that can result in extra fuel consumption. To address the lack of angular velocity measurement, the second attitude coordinated controller is given by using a novel filter. Through homogeneous method and Lyapunov theories, it is shown that the proposed controllers can achieve the finite-time stability. Numerical simulations also demonstrate that the proposed control schemes are effective. (C) 2016 IAA. Published by Elsevier Ltd. All rights reserved.

机译：本文研究了基于旋转矩阵的两种编队飞行时姿态有限控制器。因为旋转矩阵可以全局且唯一地表示一组姿态，所以两个控制器可以处理放卷，这可能导致额外的燃油消耗。为了解决角速度测量的不足，通过使用新型滤波器来提供第二姿态协调控制器。通过齐次方法和李雅普诺夫理论，证明了所提出的控制器可以达到有限时稳定性。数值模拟也表明所提出的控制方案是有效的。（C）2016 IAA。由Elsevier Ltd.出版。保留所有权利。

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来源
《Acta astronautica》 |2016年第mayajuna期|159-174|共16页
作者
Guo Yong; Song Shen-Min; Li Xue-Hui;
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作者单位

Harbin Inst Technol, Ctr Control Theory & Guidance Technol, Sci Pk,POB 3032,Yi Kuang St, Harbin 150001, Peoples R China;

Harbin Inst Technol, Ctr Control Theory & Guidance Technol, Sci Pk,POB 3032,Yi Kuang St, Harbin 150001, Peoples R China;

Harbin Inst Technol, Ctr Control Theory & Guidance Technol, Sci Pk,POB 3032,Yi Kuang St, Harbin 150001, Peoples R China;

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收录信息美国《科学引文索引》(SCI);美国《工程索引》(EI);
原文格式 PDF
正文语种 eng
中图分类
关键词
Finite-time stability; Attitude coordination control; Rotation matrix; Homogeneous method; Output feedback control;

机译：有限时间稳定性;姿态协调控制;旋转矩阵;均匀方法;输出反馈控制;

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专利

1. Finite-time output feedback control for the attitude of the spacecraft without unwinding [J] . Yong Guo, Shen-Min Song, Xue-Hui Li, Proceedings of the Institution of Mechanical Engineers . 2018,第8期

机译：不受时间限制的有限时间输出反馈控制航天器的姿态
2. Finite-time coordination control for formation flying spacecraft without unwinding [J] . Guo Yong, Song Shen-Min, Yan Zhibin Proceedings of the Institution of Mechanical Engineers . 2016,第g1期

机译：编队飞行航天器不展开的有限时间协调控制
3. Quaternion-Based Distributed Output Feedback Attitude Coordination Control for Spacecraft Formation Flying [J] . An-Min Zou, Krishna Dev Kumar Journal of guidance, control, and dynamics . 2013,第2期

机译：基于四元数的航天器编队飞行分布式输出反馈姿态协调控制
4. Finite-time attitude synchronization for spacecraft formation flying via output feedback [C] . Zhang Jian, Yan Genting, Hu Qinglei, Chinese Control Conference . 2014

机译：通过输出反馈实现航天器编队飞行的有限时间姿态同步
5. Linear and Nonlinear Adaptive Attitude Control of Asteroid-orbiting Spacecraft Using State Feedback and Output Feedback [D] . Moya, Nicholas 2018

机译：使用状态反馈和输出反馈的小行星轨道航天器的线性和非线性自适应姿态控制
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. Finite-time attitude tracking control for spacecraft without angular velocity measurements [O] . 2017

机译：没有角速度测量的航天器有限时间姿态跟踪控制

Finite-time output feedback attitude coordination control for formation flying spacecraft without unwinding

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