Design of a reduced order H∞ robust controller for an expendable launch vehicle in the presence of structured and unstructured parameter uncertainty-Reference-Cited by-同舟云学术

Design of a reduced order H∞ robust controller for an expendable launch vehicle in the presence of structured and unstructured parameter uncertainty

Published:1997-07 Issue:2 Volume:41 Page:121-130
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Xing Guang Q.,Bainum Peter M.,Li Feiyue

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference10 articles.

1. Greensite, A. L., Analysis and Design of Space Vehicle Flight Control Systems, Vol II. Macmillan, 1970

2. Pai, R. V., Bainum, P. M., Li, F. and Porada, T., in Proc. AAS/AIAA Spaceflight Mechanics Meeting, Paper AAS 95-162 edn. Albuquerque, New Mexico, 1995, pp. 13–16

3. Skelton, R. E., Dynamic System Control, Wiley, 1988

4. Xing, G. Q. and Bainum, P. M., Robust Controller Design for an Expendeble Launch Vehicle Using Normalized Coprime Factor Plant Descripta in Proceedings of the Tenth VPI & SU Symposium, ed. L. Meirovitch. Blacksburg, VA, 1995, pp. 171–180

5. Xing, G. Q. and Bainum, P. M., in 46th International Astronautical Congress, 2–6 Oct. 1995, Oslo, Norway, IAF-95-1.2.05

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