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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| வடிவமà¯: | கடà¯à®Ÿà¯à®°à¯ˆ |
| மொழி: | English |
| வெளியீடபà¯à®ªà®Ÿà¯à®Ÿà®¤à¯: |
Elsevier Masson SAS
2011
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| பகà¯à®¤à®¿à®•à®³à¯: | |
| நிகழà¯à®¨à®¿à®²à¯ˆ அணà¯à®•à®²à¯: | 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 |
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