Simultaneous spacecraft attitude and orbit estimation using magnetic field vector measurements
Based on magnetometer measurements only, three-axis attitude, rate, and orbit estimation are successfully achieved. A single Augmented Dynamics Extended Kalman Filter (ADEKF) is configured by combining the spacecraft nonlinear attitude dynamics and quaternion kinematics with orbital mechanics. The...
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Main Authors: | Mohammad Abdelrahman, Mohammad Ibraheem, Park, Sang-Young |
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Format: | Article |
Language: | English |
Published: |
Elsevier Masson SAS
2011
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Subjects: | |
Online Access: | http://irep.iium.edu.my/8582/1/b6111107506111847812c6c0b8b87987.pdf http://irep.iium.edu.my/8582/ http://www.sciencedirect.com/science/article/pii/S1270963811000186 |
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