Combined spacecraft orbit and attitude control through extended Kalman filtering of magnetometer, gyro, and GPS measurements
The main goal of this research is to establish spacecraft orbit and attitude control algorithms based on extended Kalman filter which provides estimates of spacecraft orbital and attitude states. The control and estimation algorithms must be capable of dealing with the spacecraft conditions during t...
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| Format: | Article |
| Language: | English |
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Elsevier
2014-06-01
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| Series: | Egyptian Journal of Remote Sensing and Space Sciences |
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| Online Access: | http://www.sciencedirect.com/science/article/pii/S1110982314000027 |