Autonomous Magnetic Navigation for Earth Orbiting Spacecraft

The strength and orientation of the Earth's magnetic field varies as a function of the location of the observations, which means that the magnetic field measurements contains position information. Many artificial satellites carry a magnetometer on-board. The local magnetic field measurements could be used to provide navigation information. Such a navigation method has the advantage of requiring only data from low cost on-board instruments and has applications in low budget operation of satellite systems. Furthermore if processing can be performed on-board, this method leads to the possibility of fully autonomous long term navigation. In many systems magnetic navigation could be an effective back-up. To study the feasibility and potential performance of spacecraft magnetic navigation, the concept was investigated using two possible approaches. In a first configuration the magnetic field orientation is assumed to be complemented by measurements of the Nadir direction provided by an Earth horizon sensor on board; the two vectors form the basis of a "space sextant." In the second configuration magnetic field magnitude is the sole source of external information.

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Publication Details

Journal
Digital Commons - USU (Utah State University)
Published
2025-09-10
DOI
https://doi.org/10.26077/86tq-4630
Citations
21
Primary Topic
Inertial Sensor and Navigation
Type
article
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article

Autonomous Magnetic Navigation for Earth Orbiting Spacecraft

F. Martel, Mark L. Psiaki
21 citations
Digital Commons - USU (Utah State University)
Inertial Sensor and Navigation
article

Autonomous Magnetic Navigation for Earth Orbiting Spacecraft

F. Martel, Mark L. Psiaki
article en
21 citations

Abstract

The strength and orientation of the Earth's magnetic field varies as a function of the location of the observations, which means that the magnetic field measurements contains position information. Many artificial satellites carry a magnetometer on-board. The local magnetic field measurements could be used to provide navigation information. Such a navigation method has the advantage of requiring only data from low cost on-board instruments and has applications in low budget operation of satellite systems. Furthermore if processing can be performed on-board, this method leads to the possibility of fully autonomous long term navigation. In many systems magnetic navigation could be an effective back-up. To study the feasibility and potential performance of spacecraft magnetic navigation, the concept was investigated using two possible approaches. In a first configuration the magnetic field orientation is assumed to be complemented by measurements of the Nadir direction provided by an Earth horizon sensor on board; the two vectors form the basis of a "space sextant." In the second configuration magnetic field magnitude is the sole source of external information.

Digital Commons - USU (Utah State University)
Cornell University (US)
Inertial Sensor and Navigation
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