Paper Title:
Research on Attitude Control of Spacecraft Based on ADRC
  Abstract

Modern spacecraft demands from an attitude control system very high performance and accuracy, and many new features, such as disturbance rejection capability. The recently developed active disturbance rejection control technology is applied to the attitude control of spacecraft subject to disturbances and parametric uncertainties. Simulation and experiment show significant advantages of the proposed attitude controller over the controller resulting from conventional PID approach.

  Info
Periodical
Advanced Materials Research (Volumes 383-390)
Chapter
Chapter 1: Computer-Aided Manufacturing
Edited by
Wu Fan
Pages
358-365
DOI
10.4028/www.scientific.net/AMR.383-390.358
Citation
F. L. Teng, H. Y. Ge, H. S. Li, J. H. Zhang, "Research on Attitude Control of Spacecraft Based on ADRC", Advanced Materials Research, Vols. 383-390, pp. 358-365, 2012
Online since
November 2011
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Price
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