Abstract:
This paper deals with the problem of estimating the disturbances due a wind gust in a Quadrotor rotorcraft. A linear observer with integral action for estimating the dist...Show MoreMetadata
Abstract:
This paper deals with the problem of estimating the disturbances due a wind gust in a Quadrotor rotorcraft. A linear observer with integral action for estimating the disturbance due a wind is presented. Simulation and real-time result are presented for test performance of control law proposed. The real-time test was ralized in hover fly mode based on GPS sensor signal.
Published in: 2015 12th International Conference on Electrical Engineering, Computing Science and Automatic Control (CCE)
Date of Conference: 28-30 October 2015
Date Added to IEEE Xplore: 17 December 2015
ISBN Information:
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