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2011 19th Mediterranean Conference on Control & Automation (MED)
The development of quadrotor unmanned aerial vehicles -UAVs-in potential civil applications is conditioned by the embedded elements such as removable payload, miniature actuators, sensors and power storage. As simple as the structure of the quarotor is, the dynamic behavior is complex. The paper details a model of a quadrotor which considers the effects of the location of the center of gravity and the gyroscopic torques due to the derivative of the speed propellers. A simple control law indoi:10.1109/med.2011.5983171 fatcat:swzudkilrvelhmtmlrxfnrfrum