Non-linear filter-based adaptive output feedback control for spacecraft formation flying

被引：6

作者：

Shan, J. ^{[1
]}

Lin, H. ^{[1
]}

机构：

[1] York Univ, Toronto, ON M3J 1P3, Canada

来源：

PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART I-JOURNAL OF SYSTEMS AND CONTROL ENGINEERING | 2009年 / 223卷 / I5期

关键词：

spacecraft formation flying; adaptive output control; non-linear filter;

D O I：

10.1243/09596518JSCE752

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 presents a non-linear filter-based adaptive output control for spacecraft formation flying missions. The study is motivated by the fact that only accurate position measurements are available for some systems, and velocities have to be estimated from those measurements. The proposed adaptive output controller guarantees asymptotic stability of the position and velocity tracking motion, even in the presence of uncertainties and external perturbations. The effectiveness of the proposed controller is verified by numerical simulations.

引用

页码：683 / 691

页数：9

共 48 条

[21] Prescribed-time spacecraft formation flying control with unknown disturbances by time-varying feedback
Shao, Xiaowei
Chen, Li
Chen, Junli
Zhang, Dexin
INTERNATIONAL JOURNAL OF CONTROL, 2024, 97 (11) : 2677 - 2687
[22] Adaptive High Order Sliding Mode Control for Relative Positioning and Trajectory Tracking of Spacecraft Formation Flying
Garcia Carrillo, Lois Rodolfo
Munoz Palacios, Filiberto
Espinoza Quesada, Eduardo Steed
Alexis, Kostas
2016 24TH MEDITERRANEAN CONFERENCE ON CONTROL AND AUTOMATION (MED), 2016, : 1095 - 1101
[23] Inverse optimal adaptive output feedback control of a class of Euler-Lagrange systems: A nonlinear filter based approach
Aksoy, Orhan
Zergeroglu, Erkan
Tatlicioglu, Enver
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART I-JOURNAL OF SYSTEMS AND CONTROL ENGINEERING, 2022, 236 (04) : 783 - 791
[24] Robust Adaptive Gain Higher Order Sliding Mode Observer Based Control-constrained Nonlinear Model Predictive Control for Spacecraft Formation Flying
Ranjith Ravindranathan Nair
Laxmidhar Behera
IEEE/CAAJournalofAutomaticaSinica, 2018, 5 (01) : 367 - 381
[25] Robust Adaptive Gain Higher Order Sliding Mode Observer Based Control-constrained Nonlinear Model Predictive Control for Spacecraft Formation Flying
Nair, Ranjith Ravindranathan
Behera, Laxmidhar
IEEE-CAA JOURNAL OF AUTOMATICA SINICA, 2018, 5 (01) : 367 - 381
[26] 6-DOF fixed-time adaptive tracking control for spacecraft formation flying with input quantization
Liu, Ruixia
Cao, Xibin
Liu, Ming
Zhu, Yanzheng
INFORMATION SCIENCES, 2019, 475 : 82 - 99
[27] Adaptive super-twisting sliding mode attitude coordination control for spacecraft formation flying with actuator saturation
Xiao, Chao
Guo, Yong
Xie, Cheng-qing
Li, Ai-jun
Wang, Chang-qing
ADVANCES IN SPACE RESEARCH, 2023, 72 (10) : 4244 - 4255
[28] Floquet-based design and control approach to spacecraft formation flying in libration point orbits
MENG YunHe
Science China(Technological Sciences), 2011, (03) : 758 - 766
[29] Distributed attitude consensus tracking control for spacecraft formation flying via adaptive nonsingular fast terminal sliding mode control
Xie, Xiong
Sheng, Tao
He, Liang
Chen, Zhijun
Zhao, Yong
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2022, 236 (08) : 1603 - 1616
[30] Floquet-based design and control approach to spacecraft formation flying in libration point orbits
YunHe Meng
YueDong Zhang
JinHai Dai
Science China Technological Sciences, 2011, 54 : 758 - 766

← 1 2 3 4 5 →