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http://dx.doi.org/10.5302/J.ICROS.2003.9.10.852

Equivalent Error Model for Spacecraft Attitude Determination System  

조윤철 (국방과학연구소)
유명종 (국방과학연구소)
Publication Information
Journal of Institute of Control, Robotics and Systems / v.9, no.10, 2003 , pp. 852-860 More about this Journal
Abstract
We introduce the error models for an attitude determination system(ADS) with gyroscopes and stellar sensor. The ADS error models are derived according to the definition of the reference frame and of the attitude error. The equivalent error models applicable to the attitude determination system with large attitude errors are presented. The simulation results show that the proposed error models improve performance of the attitude determination system.
Keywords
attitude determination; quaternion error model; kalman filter;
Citations & Related Records
Times Cited By KSCI : 1  (Citation Analysis)
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