Share Email Print

Proceedings Paper

QFT/H∞ robust mixed sensitivity control of command tracking system for space vehicle
Author(s): Changwei Yang; Jinwen An
Format Member Price Non-Member Price
PDF $14.40 $18.00
cover GOOD NEWS! Your organization subscribes to the SPIE Digital Library. You may be able to download this paper for free. Check Access

Paper Abstract

This paper describes a QFT/H design method which combines the Quantitative Feedback Theory (QFT) design concept and robust H optimal control technique via linear matrix inequality (LMI) convex optimization approach. The relationship between QFT and H robust control of tracking systems will be discussed. Based on our extensive experience with both H and QFT design approaches, it appears reasonable that by synthesizing both into a single design process and enjoying the benefits offered by each approach. The complexity of the robust control system design for space vehicle is decreased by combined QFT/H design technique. Furthermore the robust controller of command tracking system is designed by QFT/H method using the advantages of the two methods for space vehicle, and the results of design are validated through simulations.

Paper Details

Date Published: 10 November 2007
PDF: 7 pages
Proc. SPIE 6795, Second International Conference on Space Information Technology, 67956T (10 November 2007); doi: 10.1117/12.775235
Show Author Affiliations
Changwei Yang, Northwestern Polytechnical Univ. (China)
Jinwen An, Northwestern Polytechnical Univ. (China)

Published in SPIE Proceedings Vol. 6795:
Second International Conference on Space Information Technology
Cheng Wang; Shan Zhong; Jiaolong Wei, Editor(s)

© SPIE. Terms of Use
Back to Top