Control strategy for the transition flight of a tail-sitter UAV

The tail-sitter unmanned aerial vehicle (UAV) is a kind of vertical take-off and landing (VTOL) UAV which has the merits of both fixed-wing and rotary-wing. The tail-sitter UAV in this paper has three flight modes. The most important stage is the transition stage. The model for the transition stage is established and a transition flight strategy is constructed so that the UAV can change vertical takeoff mode to cruise mode stably. A nonlinear extended state observer is presented to estimate the unknown nonlinear terms, the uncertainties and external disturbances during mode transition. The backstepping controller based on the observer is designed to implement transition flight mode. A numerical simulation is given to demonstrate the effectiveness of the obtained results.