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...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
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Elsevier Masson SAS
2011
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/8582/ http://irep.iium.edu.my/8582/ http://irep.iium.edu.my/8582/ http://irep.iium.edu.my/8582/1/b6111107506111847812c6c0b8b87987.pdf |