QFT design for spacecraft with uncertain flexible structures

Wen Hua Chen

doi:10.1109/WCICA.2006.1713571

QFT design for spacecraft with uncertain flexible structures

Department of Aeronautical and Aviation Engineering

Research output: Chapter in book / Conference proceeding › Conference article published in proceeding or book › Academic research › peer-review

3 Citations (Scopus)

Abstract

Future space missions require spacecraft with large flexible structures which imposes a quite challenging design problem for attitude and orbit control systems (AOCS). This paper investigates the robust control problem of Darwin flyer benchmark using quantitative feedback theory (QFT). After representing the design specifications into explicit and implicit design criteria in QFT design environment, the 6 degrees of freedom design problem is re-formulated as a design problem for 6 SISO uncertain plants and the corresponding controllers are designed using loop shaping. The designed controllers are tested on the fully coupled benchmark simulator with significant uncertainties, and satisfactory performance is demonstrated.

Original language	English
Title of host publication	Proceedings of the World Congress on Intelligent Control and Automation (WCICA)
Pages	8191-8195
Number of pages	5
DOIs	https://doi.org/10.1109/WCICA.2006.1713571
Publication status	Published - 2006
Event	6th World Congress on Intelligent Control and Automation, WCICA 2006 - Dalian, China Duration: 21 Jun 2006 → 23 Jun 2006

Publication series

Name	Proceedings of the World Congress on Intelligent Control and Automation (WCICA)
Volume	2

Conference

Conference	6th World Congress on Intelligent Control and Automation, WCICA 2006
Country/Territory	China
City	Dalian
Period	21/06/06 → 23/06/06

Keywords

Flexible structures
Quantitative feedback theory
Robust control
Spacecraft

ASJC Scopus subject areas

Control and Systems Engineering
Software
Computer Science Applications

More information

10.1109/WCICA.2006.1713571

Cite this

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Chen, WH 2006, QFT design for spacecraft with uncertain flexible structures. in Proceedings of the World Congress on Intelligent Control and Automation (WCICA)., 1713571, Proceedings of the World Congress on Intelligent Control and Automation (WCICA), vol. 2, pp. 8191-8195, 6th World Congress on Intelligent Control and Automation, WCICA 2006, Dalian, China, 21/06/06. https://doi.org/10.1109/WCICA.2006.1713571

QFT design for spacecraft with uncertain flexible structures. / Chen, Wen Hua.
Proceedings of the World Congress on Intelligent Control and Automation (WCICA). 2006. p. 8191-8195 1713571 (Proceedings of the World Congress on Intelligent Control and Automation (WCICA); Vol. 2).

Research output: Chapter in book / Conference proceeding › Conference article published in proceeding or book › Academic research › peer-review

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QFT design for spacecraft with uncertain flexible structures

Abstract

Publication series

Conference

Keywords

ASJC Scopus subject areas

More information

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