FAULT TOLERANT ATTITUDE CONTROL DURING FORMATION FLYING

被引：0

作者：

Li, Junquan ^{[1
]}

Kumar, K. D. ^{[2
]}

机构：

[1] Ryerson Univ, Dept Aerosp Engn, 350 Victoria St, Toronto, ON M58 2K3, Canada

[2] Ryerson Univ, Dept Aerosp Engn, Space Syst, Toronto, ON M58 2K3, Canada

来源：

SPACEFLIGHT MECHANICS 2010, PTS I-III | 2010年 / 136卷

关键词：

SLIDING MODE-CONTROL; SPACECRAFT; SYSTEMS;

D O I：

暂无

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

The authors propose an adaptive fuzzy terminal sliding mode control algorithm (AFTSMC) for attitude tracking of multiple picosatellites during formation flying. The relative attitude of the leader and follower picosatellites under gravity gradient torque and external periodic disturbances is controlled by four reaction wheels. This method can accommodate faults rapidly without controller reconfiguration. The numerical simulations (under the fault and failure of wheel) demonstrate the effectiveness of the proposed controllers.

引用

页码：1933 / +

页数：4

共 50 条

[11] Fault Tolerant Control of Attitude Dynamics of Nanosatellites
Guler, Demet Cilden
Hajiyev, Chingiz
Dasdemir, Janset
PROCEEDINGS OF 8TH INTERNATIONAL CONFERENCE ON RECENT ADVANCES IN SPACE TECHNOLOGIES (RAST 2017), 2017, : 349 - 353
[12] Orbit and attitude control of spacecraft formation flying
张治国
李俊峰
Applied Mathematics and Mechanics(English Edition), 2008, (01) : 43 - 50
[13] Attitude tracking control for satellite formation flying
Zhang, Zhiguo
Li, Junfeng
Baoyin, Hexi
Qinghua Daxue Xuebao/Journal of Tsinghua University, 2006, 46 (11): : 1914 - 1917
[14] Orbit and attitude control of spacecraft formation flying
Zhang Zhi-guo
Li Jun-feng
APPLIED MATHEMATICS AND MECHANICS-ENGLISH EDITION, 2008, 29 (01) : 43 - 50
[15] Orbit and attitude control of spacecraft formation flying
Zhi-guo Zhang
Jun-feng Li
Applied Mathematics and Mechanics, 2008, 29 : 43 - 50
[16] 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
[17] Fault diagnosis and fault tolerant control for nonlinear satellite attitude control systems
Gao, Chunyan
Duan, Guangren
AEROSPACE SCIENCE AND TECHNOLOGY, 2014, 33 (01) : 9 - 15
[18] Robust Adaptive Fault-tolerant Attitude Control of Flying-wing UAVs with Flight Envelope Constraints
Yu Z.
Li Y.
Pei B.
Xu W.
Duan X.
Song K.
Binggong Xuebao/Acta Armamentarii, 2024, 45 (01): : 231 - 240
[19] Composite continuous nonsingular terminal sliding mode fault tolerant attitude tracking control for flying wing UAV
Zhao Z.-H.
Gu Z.-X.
Xue P.-X.
Cao D.
Zu J.-K.
Kongzhi Lilun Yu Yingyong/Control Theory and Applications, 2023, 40 (07): : 1277 - 1286
[20] Reconfigurable Fault-Tolerant Control for Spacecraft Formation Flying Based on Iterative Learning Algorithms
Gui, Yule
Jia, Qingxian
Li, Huayi
Cheng, Yuehua
APPLIED SCIENCES-BASEL, 2022, 12 (05):

← 1 2 3 4 5 →