Gain-scheduled extended Kalman filter for nanosatellite attitude determination system
Extended Kalman filter (EKF) has been widely used for attitude determination in various satellite missions. However, it requires an extensive computational power which is not suitable for nano-satellite application. This paper proposes a gain-scheduled EKF (GSEKF) to reduce the computational require...
| Main Authors: | , , , |
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| Other Authors: | |
| Format: | Journal Article |
| Language: | English |
| Published: |
2015
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| Subjects: | |
| Online Access: | https://hdl.handle.net/10356/79372 http://hdl.handle.net/10220/38331 |