The invention provides a flight control
simulation system with fault diagnosis capability for an unmanned helicopter. The flight control
simulation system with fault diagnosis capability for an unmanned helicopter comprises a
simulation general control console, a simulation computer, a flight control
management system, a
sensor system, physical effect equipment, a
servo system, a
remote control and remote measurement system, and a task load system, wherein the simulation general control console controls the simulation computer to carry on a power on test, model generation and injection of
fault model; the simulation computer selects simulation and interference model and simulates
fault injection to carry on flight simulation; the flight control
management system receives the information of sensors and the
remote control and remote measurement system; the
servo system realizes the real reaction of an operating mechanism; and the
sensor system transmits the acquired sensor information to the flight control
management system. For the flight control
simulation system with fault diagnosis capability for an unmanned helicopter, the simulation computer can be embedded into different aircraft mathematical models, so that simulation of a plurality of aircrafts can be realized. For the flight control
simulation system with fault diagnosis capability for an unmanned helicopter, the
servo system and the
sensor system can access a real steering engine of aircraft and real sensors so as to develop the steering engine of aircraft, to make a test flight for the steering engine of aircraft, and detecting working of the sensors.