The Research of Micro-Satellite Attitude Determination Based on Predictive Filter

Lu Cao; Wei Wei Yang; Xiao Qian Chen; Yi Yong Huang

doi:10.4028/www.scientific.net/AMM.110-116.5413

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 110-116The Research of Micro-Satellite Attitude...

The Research of Micro-Satellite Attitude Determination Based on Predictive Filter

Abstract:

— An extended predictive filter is presented for attitude determination of Micro-satellite based on the basic theory of predictive filter. This algorithm enhances the precision of kinematics equation, accurately estimates satellite attitude angle and angular velocity using measurement vectors from magnetometer and sun sensors by predicting model errors and angular velocity errors one step ahead. In addition, a new measurement model is derived about angular velocity, which improved the efficiency of the use of measurement vectors. Simulation results show both the high reliability and precision of this method.

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Periodical:

Applied Mechanics and Materials (Volumes 110-116)

Pages:

5413-5419

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.110-116.5413

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Online since:

October 2011

Authors:

Lu Cao, Wei Wei Yang, Xiao Qian Chen, Yi Yong Huang

Keywords:

Angular Velocity, Attitude Determination, Model Error, Predictive Filter

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