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• W2144585741 abstract "This paper presents the design of an estimation algorithm for the determination of a low-Earth satellite orbitbased only on the measurements of the Earth magnetic field. The algorithm is based on the extended Kalmanfilter (EKF) and the measure of the magnitude of the magnetic field, which provides an estimation methodindependent of the satellite attitude. The satellite orbit is described with a state vector formed by the classicalKeplerian orbital elements. The simulation test resulted in an accurate estimation of the state vectorcomponents and yielded only a few kilometres error on the satellite position. The effect of the variation of theorbit inclination and eccentricity on the filter performances was also investigated." @default.
• W2144585741 created "2016-06-24" @default.
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• W2144585741 creator A5074383707 @default.
• W2144585741 date "2006-01-01" @default.
• W2144585741 modified "2023-09-27" @default.
• W2144585741 title "Satellite orbit estimation using earth magnetic field measurements" @default.
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• W2144585741 hasPublicationYear "2006" @default.
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