An orbit determination algorithm with onboard GPS using kalman filter

Details An orbit determination algorithm with onboard GPS using kalman filter An orbit determination algorithm with onboard GPS using kalman filter

Oct 2005

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2005acasn..46..441j&link_type=abstract

Acta Astronomica Sinica, vol. 46, no. 4, p. 441-451

Astronomy and Astrophysics

Astronomy

2

Gps, Kalman Filter, Autonomous Orbit Determination

Scientific paper

Kalman filter is used in the orbit determination of Shenzou 4 with on-board GPS data. The study is mainly on three problems: the choice of variance matrix of model noise, the influence of signal interrupt or continuous outliers to the recursion filter and the method of monitoring the running status (normal or divergence) of the filter. The aim is to evaluate the reliability of this algorithm for the long-time on-board autonomous orbit determination.

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