Adaptive finite-time attitude stabilization for rigid spacecraft with actuator faults and saturation constraints-Reference-Cited by-同舟云学术

Adaptive finite-time attitude stabilization for rigid spacecraft with actuator faults and saturation constraints

Published:2015-01-19 Issue:1 Volume:26 Page:28-46
ISSN:1049-8923
Container-title:International Journal of Robust and Nonlinear Control
language:en
Short-container-title:Int. J. Robust. Nonlinear Control

Author:

Lu Kunfeng¹²,Xia Yuanqing³,Fu Mengyin³,Yu Chunmei¹²

Affiliation:

1. Beijing Aerospace Automatic Control Institute; Beijing 100854 China

2. National Key Laboratory of Science and Technology on Aerospace Intelligent Control; Beijing 100854 China

3. School of Automation; Beijing Institute of Technology; Beijing 100081 China

Publisher

Wiley

Subject

Electrical and Electronic Engineering,Industrial and Manufacturing Engineering,Mechanical Engineering,Aerospace Engineering,Biomedical Engineering,General Chemical Engineering,Control and Systems Engineering

Reference34 articles.

1. Globally stabilizing proportional-integral-derivative control laws for rigid-body attitude tracking;Su;Journal of Guidance, Control, and Dynamics,2011

2. Inverse optimal adaptive control for attitude tracking of spacecraft;Luo;IEEE Transactions on Automatic Control,2005

3. Attitude tracking and disturbance rejection of rigid spacecraft by adaptive control;Chen;IEEE Transactions on Automatic Control,2009

4. PD+based output feedback attitude control of rigid bodies;Schlanbusch;IEEE Transactions on Automatic Control,2012

5. Attitude stabilization of spacecrafts under actuator saturation and partial loss of control effectiveness;Xiao;IEEE Transactions on control systems technology,2013

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