AFFINE MOTION CONTROL MODEL FOR UAV TRI-ROTORS

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Abstract

In this paper, the Tri-rotor dynamical model to transform it to affine form control system model, which is easier to apply the modern control theories to synthesize the Tri-rotor UAV control law is analyzed. A specific Tri-rotor UAV’s model is selected, the Matlab-Simulink to simulate the steady-state motion in space to demonstrate the correctness of this model is used.