Disturbance Rejection in UAV's velocity and attitude control: Problems and solutions

@article{Xiong2011DisturbanceRI,
  title={Disturbance Rejection in UAV's velocity and attitude control: Problems and solutions},
  author={Hua Xiong and Ruyi Yuan and Jianqiang Yi and Guoliang. Fan and Fengshui Jing},
  journal={Proceedings of the 30th Chinese Control Conference},
  year={2011},
  pages={6293-6298}
}
For the high nonlinearity and coupling of the model of the Unmanned Aerial Vehicles (UAVs), the control of velocity and attitude (i.e. pitch angle, roll angle, and yaw angle) under various disturbances (e.g. wind disturbances) has been a challenging research all along. In this paper, we confirm that under some simplifications the throttle-velocity subsystem is of first-order, the elevator-pitch angle subsystem, the aileron-roll angle subsystem, and the rudder-yaw angle subsystem are of second… CONTINUE READING
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