Simulation Research on the Rendezvous and Guidance Law of Fixed-Wing Unmanned Aerial Vehicles for Aerial Targets

The application of the guidance law to the rendezvous of aerial targets of fixed-wing unmanned aerial vehicles was proposed. To complete the aerial rendezvous of fixed-wing unmanned aerial vehicles (UAVs) and rotary-wing UAVs, simulation analysis and research on the guidance parameters of the initial guidance and proportional guidance stages were carried out respectively. In the initial guidance stage, this guidance law mainly focuses on linear motion to quickly approach the target position. In the proportional guidance stage, the velocity direction of the fixed-wing UAVs is corrected by the proportional coefficient. Enable fixed-wing unmanned aerial vehicles to complete aerial rendezvous. Through the simulation research of the maneuvering models of some types of rotorcraft unmanned aerial vehicles, this guidance law can effectively complete the rendezvous of aerial targets.