Unmanned aerial vehicle (UAV) has become a research hotspot because of its wide application in civil and military fields. For UAV with aerodynamic configuration

the rotation per degree of freedom is controlled by the operator interface. Modern high-performance UAVs typically camouflage and survive on multiple control surfaces and unconventional aerodynamic s construction. The main problem of UAV flight control system design is to solve the problem of full distribution and survival of UAV. Coordinate multiple workfaces controls and use redundancy for maximum control efficiency. Control assignment technology allows different flight conditions. The research on ground control technology of multi-function UAV has important theoretical significance and application value. The research results can also be used in the control design of other overdrive systems (ships

submarines

etc.).