Attitude tracking of rigid spacecraft subject to disturbances of unknown frequencies-Reference-Cited by-同舟云学术

Attitude tracking of rigid spacecraft subject to disturbances of unknown frequencies

Published:2013-03-25 Issue:16 Volume:24 Page:2231-2242
ISSN:1049-8923
Container-title:International Journal of Robust and Nonlinear Control
language:en
Short-container-title:Int. J. Robust. Nonlinear Control

Author:

Chen Zhiyong¹,Huang Jie²

Affiliation:

1. School of Electrical Engineering and Computer Science; The University of Newcastle; Callaghan NSW 2308 Australia

2. Department of Mechanical and Automation Engineering; The Chinese University of Hong Kong; Shatin, N.T. Hong Kong 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

Reference23 articles.

1. Adaptive asymptotic tracking of spacecraft attitude motion with inertia matrix identification;Ahmed;Journal of Guidance, Control and Dynamics,1998

2. Spacecraft adaptive attitude and power tracking with variable speed control moment gyroscopes;Yoon;Journal of Guidance, Control and Dynamics,2002

3. Unit quaternion-based output feedback for the attitude tracking problem;Tayebi;IEEE Transactions on Automatic Control,2008

4. Attitude control of missile via fliess expansion;Yao;IEEE Transactions on Control Systems Technology,2008

5. Stabilization of the attitude of a rigid spacecraft with external disturbances using finite-time control techniques;Ding;Aerospace Science And Technology,2009

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