Abstract:Aiming at the problems of wind disturbance and actuator input constraints during the formation flight of fixed-wing unmanned aerial vehicles (UAVs), a distributed cooperative control method with virtual leader is designed. The kinematics model of UAVs in wind field environment is established, and a smooth function which can deal with asymmetric upper and lower bounds is used to limit the input. The consistent formation control law of trajectory tracking under constant wind disturbance and input constraints is derived by state feedback. Furthermore, considering random wind disturbance, a robust sliding mode formation control law with input constraints is designed. The simulation results show that compared with traditional algorithms, the proposed formation control law can achieve wind-resistant trajectory tracking formation flying under input constraints, and has faster convergence speed and higher control accuracy.