Autonomous Navigation of MegSat1: Attitude, Sensor Bias and Scale Factor Estimation by EKF and Magnetometer-Only Measurement-Reference-Cited by-同舟云学术

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Autonomous Navigation of MegSat1: Attitude, Sensor Bias and Scale Factor Estimation by EKF and Magnetometer-Only Measurement

Published:2004-05-09 Issue: Volume: Page:
ISSN:
Container-title:22nd AIAA International Communications Satellite Systems Conference & Exhibit 2004 (ICSSC)
language:
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Author:

Da Forno Roberto,Reali Fabrizio,Bristot Stefano,Debei Stefano

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-3183

Reference7 articles.

1. Kalman Filtering for Spacecraft Attitude Estimation

2. Three-axis attitude determination via Kalman filtering of magnetometer data

3. 3Natanson,G.A.,etal."ADeterministicMethodforEstimatingAttitudeFromMagnetometerDataOnly",papern.IAF-92-0036,Proc.af theWorldSpaceCongress, Washington, DC,Sept.1992, pp.1-13.

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