Dual Extended Kalman Filter Based Momentum Wheel Identification

Zhi Zhou Li; Rui Zhang; Zhen Cai Zhu; Xu Wen Liang

doi:10.4028/www.scientific.net/AMM.29-32.2278

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 29-32Dual Extended Kalman Filter Based Momentum Wheel...

Dual Extended Kalman Filter Based Momentum Wheel Identification

Abstract:

As the most important actuator of the attitude control subsystem of the spacecraft, the momentum wheel should be precisely simulated. In this paper, Dual Extended Kalman filter is expressed and used to identify the momentum wheel system. In this way, the identification result can be used in the momentum wheel system simulation. This makes simulations run both fast and precisely. The numerical simulation results show that the algorithm can converge in given error.

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Periodical:

Applied Mechanics and Materials (Volumes 29-32)

Pages:

2278-2284

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.29-32.2278

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Cite this paper

Online since:

August 2010

Authors:

Zhi Zhou Li, Rui Zhang, Zhen Cai Zhu, Xu Wen Liang

Keywords:

Attitude Control System, Kalman Filter (KF), Momentum Wheel, System Identification

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