A hybrid control scheme of adaptive and variable structure for flexible spacecraft-Reference-Cited by-同舟云学术

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A hybrid control scheme of adaptive and variable structure for flexible spacecraft

Published:2004-07 Issue:5 Volume:8 Page:423-430
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Li Zhi-Bin,Wang Zhao-Lin,Li Jun-Feng

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference10 articles.

1. A dynamics Parameter Invariant Attitude Control System for Flexible Spacecraft Dynamics of Flexible Structures in Space;Dodds,1990

2. The Fundamental of Variable Structure Control Theory;Gao,1990

3. On intelligent adaptive control of a type spacecraft;Li;Chinese Space Sci. Technol.,1998

4. A type of variable parameter experimental system with deployable flexible structure;Li;J. Astronautics,2001

5. Variable-structure control of spacecraft large-angle maneuvers;Vadali;J. Guidance,1986

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2. Modeling and co-simulating of a large flexible satellites with three reaction wheels in ADAMS and MATLAB;International Journal of Dynamics and Control;2017-01-28

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