Magnetic-Only Orbit and Attitude Estimation Using the Square-Root Unscented Kalman Filter: Application to the PROBA-2 Spacecraft-Reference-Cited by-同舟云学术

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Magnetic-Only Orbit and Attitude Estimation Using the Square-Root Unscented Kalman Filter: Application to the PROBA-2 Spacecraft

Published:2008-06-15 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation and Control Conference and Exhibit
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Author:

Côté JImmy¹,de Lafontaine Jean¹

Affiliation:

1. NGC Aerospace Ltd

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-6293

Reference24 articles.

1. T. Bak, "Spacecraft Attitude Determination- a Magnetometer Approach". PhD Thesis,Aalborg University, Departmentof Control Engineering,1999

2. Orbit Determination Using the Geomagnetic Field Measurement via the Unscented Kalman Filter

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3. Robust unscented Kalman filter for nanosat attitude estimation;International Journal of Control, Automation and Systems;2017-09-06

4. Magnetometer-only attitude and angular velocity filtering estimation for attitude changing spacecraft;Acta Astronautica;2014-09

5. An improved quaternion Gauss–Newton algorithm for attitude determination using magnetometer and accelerometer;Chinese Journal of Aeronautics;2014-08

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