Satellite orbit estimation using earth magnetic field measurements

This paper presents the design of an estimation algorithm for the determination of a low-Earth satellite orbit based only on the measurements of the Earth magnetic field. The algorithm is based on the extended Kalman filter (EKF) and the measure of the magnitude of the magnetic field, which provid...

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Main Authors: Filipski, Mohammad Nizam, Varatharajoo, Renuganth
Format: Conference or Workshop Item
Language:English
Published: Federation of Engineering Institutions of Islamic Countries 2006
Online Access:http://psasir.upm.edu.my/id/eprint/39480/
http://psasir.upm.edu.my/id/eprint/39480/1/39480.pdf
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author Filipski, Mohammad Nizam
Varatharajoo, Renuganth
author_facet Filipski, Mohammad Nizam
Varatharajoo, Renuganth
author_sort Filipski, Mohammad Nizam
building UPM Institutional Repository
collection Online Access
description This paper presents the design of an estimation algorithm for the determination of a low-Earth satellite orbit based only on the measurements of the Earth magnetic field. The algorithm is based on the extended Kalman filter (EKF) and the measure of the magnitude of the magnetic field, which provides an estimation method independent of the satellite attitude. The satellite orbit is described with a state vector formed by the classical Keplerian orbital elements. The simulation test resulted in an accurate estimation of the state vector components and yielded only a few kilometres error on the satellite position. The effect of the variation of the orbit inclination and eccentricity on the filter performances was also investigated.
first_indexed 2025-11-15T09:45:53Z
format Conference or Workshop Item
id upm-39480
institution Universiti Putra Malaysia
institution_category Local University
language English
last_indexed 2025-11-15T09:45:53Z
publishDate 2006
publisher Federation of Engineering Institutions of Islamic Countries
recordtype eprints
repository_type Digital Repository
spelling upm-394802015-07-22T03:45:05Z http://psasir.upm.edu.my/id/eprint/39480/ Satellite orbit estimation using earth magnetic field measurements Filipski, Mohammad Nizam Varatharajoo, Renuganth This paper presents the design of an estimation algorithm for the determination of a low-Earth satellite orbit based only on the measurements of the Earth magnetic field. The algorithm is based on the extended Kalman filter (EKF) and the measure of the magnitude of the magnetic field, which provides an estimation method independent of the satellite attitude. The satellite orbit is described with a state vector formed by the classical Keplerian orbital elements. The simulation test resulted in an accurate estimation of the state vector components and yielded only a few kilometres error on the satellite position. The effect of the variation of the orbit inclination and eccentricity on the filter performances was also investigated. Federation of Engineering Institutions of Islamic Countries 2006 Conference or Workshop Item NonPeerReviewed application/pdf en http://psasir.upm.edu.my/id/eprint/39480/1/39480.pdf Filipski, Mohammad Nizam and Varatharajoo, Renuganth (2006) Satellite orbit estimation using earth magnetic field measurements. In: Seminar on Engineering and Technology (SET2006) , 4-5 Sept. 2006, Putrajaya, Malaysia. (pp. 163-171).
spellingShingle Filipski, Mohammad Nizam
Varatharajoo, Renuganth
Satellite orbit estimation using earth magnetic field measurements
title Satellite orbit estimation using earth magnetic field measurements
title_full Satellite orbit estimation using earth magnetic field measurements
title_fullStr Satellite orbit estimation using earth magnetic field measurements
title_full_unstemmed Satellite orbit estimation using earth magnetic field measurements
title_short Satellite orbit estimation using earth magnetic field measurements
title_sort satellite orbit estimation using earth magnetic field measurements
url http://psasir.upm.edu.my/id/eprint/39480/
http://psasir.upm.edu.my/id/eprint/39480/1/39480.pdf