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Satellite Attitude Estimation UKF Algorithm Based on Star-Sensor

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3 Author(s)
Hui Li ; Research Centre of Satellite Technology, Harbin Institute of Technology, Harbin 150001, China. Phone: + 86-451-8640 2357, Fax: +86-451-8641 6547, E-mail: ; Zhao-wei Sun ; Shi-jie Zhang

The objective of this paper is to derive a satellite attitude estimation algorithm only using vector observation from the star-sensor, in gyros-less or gyro-disable mode. State estimation is achieved through the unscented Kalman filter (UKF) based on unscented transformation. Simulation results indicate that this approach is feasible and effective

Published in:

Computational Engineering in Systems Applications, IMACS Multiconference on  (Volume:1 )

Date of Conference:

4-6 Oct. 2006