Paper Title:
Fuzzy Adaptive Variable Structure Active Attitude Control of Flexible Spacecraft
  Abstract

This paper presents a novel control system design method for the three-axis-rotational tracking and vibration stabilization of a spacecraft with flexible appendages. Based on the sliding control theory, a robust attitude control law is derived to control the attitude motion of spacecraft. For actively suppressing the induced vibration, both fuzzy methods and strain rate feedback (SRF) control methods are presented. Numerical simulations are performed to show the feasibility and effeteness of the proposed methods.

  Info
Periodical
Edited by
Ran Chen
Pages
2070-2074
DOI
10.4028/www.scientific.net/AMM.44-47.2070
Citation
F. Y. Qu, L. K. Zhu, W. L. Song, "Fuzzy Adaptive Variable Structure Active Attitude Control of Flexible Spacecraft", Applied Mechanics and Materials, Vols. 44-47, pp. 2070-2074, 2011
Online since
December 2010
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