Research on Flight Control Simulation System of UAV

The scheme of developing a UAV simulation system is proposed regarding the research of concern type.Firstly,the validity of fight control laws is verified by the simulation test with full digital mode.Based on the validity course,two correlative semi-physical simulation systems are both designed according to different conditions to simulate flight status of UAV,which are separated with turntable function and without turntable function.Finally,partial curves of simulation are illustrated.The simulation results show that rationality and effectiveness of UAV FCS design are achieved based on proposed simulation system.Meanwhile,it can serve as a reference for designing simulation system of the congener aircraft.