Paper Title:
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.

  Info
Periodical
Chapter
Chapter 24: Semiconductor Materials Manufacturing
Edited by
Wu Fan
Pages
5413-5419
DOI
10.4028/www.scientific.net/AMM.110-116.5413
Citation
L. Cao, W. W. Yang, X. Q. Chen, Y. Y. Huang, "The Research of Micro-Satellite Attitude Determination Based on Predictive Filter", Applied Mechanics and Materials, Vols. 110-116, pp. 5413-5419, 2012
Online since
October 2011
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