Nonlinear Extended Kalman Filter for Attitude Estimation of the Fixed-Wing UAV
Flying vehicle’s navigation, direction, and control in real-time results in the design of a strap-down inertial navigation system (INS). The strategy results in low accuracy, performance with correctness. Aiming at the attitude estimation problem, many data fusion or filtering methods had been appli...
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| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Wiley
2022-01-01
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| Series: | International Journal of Optics |
| Online Access: | http://dx.doi.org/10.1155/2022/7883851 |
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