Conference Paper

Inspection UAV landing navigation system by fusing UWB information and height data

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A new method to estimate the aircraft heading angle, wind velocity, and airspeed bias error is proposed without relying on the magnetometer. A GPS, rate-gyro, pitot-static tube, and sideslip angle sensor are combined through a design of an extended Kalman filter based on a vectorial geometric relation among the ground, air, and wind velocity. The feasibility of the method is validated through a desktop simulation. The flight test is conducted utilizing the estimated yaw angle as a guidance variable to evaluate the performance of the method. The estimated wind information is compared to the automatic weather system nearby.
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Review on UAV intelligent technology for transmission
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X. R. Miao, Z. Y. Liu, and Q. C. Yan. "Review on UAV intelligent technology for transmission." Journal of Fuzhou University (Natural Science Edition), 2020, 48(02): 198-209.
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