Robust Approach to Attitude Control and Momentum Management for Space Station

Bing Han; Wei Huo

doi:10.4028/www.scientific.net/AMM.644-650.578

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 644-650Robust Approach to Attitude Control and Momentum...

Robust Approach to Attitude Control and Momentum Management for Space Station

Abstract:

A novel methodology to design a robust attitude control and momentum management controller for the space station is proposed. Firstly, the method of maximum rank decomposition is adopted to deal with parameter uncertainties independently. Secondly, based on the resulted model, an optimal controller, with closed-loop region pole constraints, is designed. Finally, simulation results are presented to demonstrate the control effects.

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Periodical:

Applied Mechanics and Materials (Volumes 644-650)

Pages:

578-585

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.644-650.578

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Online since:

September 2014

Authors:

Bing Han*, Wei Huo

Keywords:

Attitude Control, H_∞ Control, Momentum Management, Space Station

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