Bounded error identification of the wind gusts effect on a small-scaled helicopter
This paper is dealing with the problem of estimating the effects of wind gusts on a small helicopter type UAV. A model of the UAV is first described, including potential effects of wind. Identification of the state vector representing the UAV is performed using a set estimation technique in order to characterize the variation boundaries of the flight induced by the presence of wind. Simulation results are presented to illustrate the identification performance.