Abstract: | From the engineering-development viewpoint,the system configuration,main functions,outer interface and structure of typical unmanned aerial vehicle(UAV) flight control and management systems(FCMS) are intro-duced first.Then,the main problems of system function design of flight control,mission management,airborne equipment failure diagnose and payload management,et al.are analyzed.Thirdly,the characteristics and applicabili-ties of three typical control modes,i.e.remote pilot,automatic control under man-surveillance and autonomous con-trol are discussed.And then,the key technologies in system development such as control law design,control and management strategy design,real-time software development,et al.are analyzed.Finally,the system characteristics obtained from manned aerial vehicles and system development trends are induced. |