A Thruster Layout Scheme for Fault-Tolerant Attitude Control of Spacecraft

被引：1

作者：

Zhang, Feng ^{[1
]}

Tang, Qiong ^{[1
]}

Wang, Shuting ^{[1
]}

Li, Yang ^{[1
]}

Yan, Ning ^{[1
]}

机构：

[1] China Acad Launch Vehicle Technol, Res & Dev Dept, Beijing, Peoples R China

来源：

2020 CHINESE AUTOMATION CONGRESS (CAC 2020) | 2020年

基金：

中国国家自然科学基金;

关键词：

thruster layout; fault-tolerant capability; attitude control; TRACKING;

D O I：

10.1109/CAC51589.2020.9327257

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

This paper deals with the fault-tolerant thruster layout design problem for three-axis attitude control of spacecraft. To do so, a novel thruster layout scheme is proposed to improve the fault-tolerant capability of the three-axis attitude control of spacecraft. Four types of possible cases of thruster failures are analyzed and the corresponding control allocation strategy is corrected based on the given thruster layout. Moreover, the comparison of the fault-tolerant capability caused by the traditional and the proposed thruster layout schemes are conducted via numerical analysis to verify the effectiveness and the advantages of the proposed scheme.

引用

页码：3863 / 3866

页数：4

共 50 条

[31] Spacecraft attitude fault-tolerant control based on iterative learning observer and control allocation
Hu, Qinglei
Niu, Guanglin
Wang, Chenliang
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 75 : 245 - 253
[32] Adaptive Fault-Tolerant Attitude-Tracking Control of Spacecraft With Quantized Control Torque
Yuan, Zhi
Wu, Lina
Yao, Xiuming
IEEE ACCESS, 2020, 8 : 226653 - 226661
[33] Fault-Tolerant Attitude Control for Rigid Spacecraft Without Angular Velocity Measurements
Wang, Xianghua
Tan, Chee Pin
Wu, Fen
Wang, Jiandong
IEEE TRANSACTIONS ON CYBERNETICS, 2021, 51 (03) : 1216 - 1229
[34] Fault-tolerant attitude control for flexible spacecraft subject to input and state constraint
Golestani, Mehdi
Esmaeilzadeh, Seyed Majid
Xiao, Bing
TRANSACTIONS OF THE INSTITUTE OF MEASUREMENT AND CONTROL, 2020, 42 (14) : 2660 - 2674
[35] Fault-Tolerant Reduced-Attitude Control for Spacecraft Constrained Boresight Reorientation
Shao, Xiaodong
Hu, Qinglei
Zhu, Zheng H.
Zhang, Youmin
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2022, 45 (08) : 1481 - 1495
[36] Hybrid Attitude Saturation and Fault-Tolerant Control for Rigid Spacecraft without Unwinding
Ma, Jun
Wang, Zeng
Wang, Chang
MATHEMATICS, 2023, 11 (15)
[37] Adaptive fault-tolerant attitude tracking control for spacecraft formation with unknown inertia
Zhu, Zhihao
Guo, Yu
INTERNATIONAL JOURNAL OF ADAPTIVE CONTROL AND SIGNAL PROCESSING, 2018, 32 (01) : 13 - 26
[38] Robust fault-tolerant control for spacecraft attitude stabilisation subject to input saturation
Hu, Q.
Xiao, B.
Friswell, M. I.
IET CONTROL THEORY AND APPLICATIONS, 2011, 5 (02): : 271 - 282
[39] Fixed-Time Fault-Tolerant Attitude Tracking Control for Rigid Spacecraft
Wang, Zeng
Su, Yuxin
Zhang, Liyin
JOURNAL OF DYNAMIC SYSTEMS MEASUREMENT AND CONTROL-TRANSACTIONS OF THE ASME, 2020, 142 (02):
[40] Sliding-mode fault-tolerant attitude control for spacecraft using SGCMGs
Zhang F.
Jin L.
Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics, 2017, 43 (04): : 806 - 813

← 1 2 3 4 5 →