Design of Automatic Flight Track Generator

The verification of inertial navigation algorithms and flight control laws needs the flight track data and the corresponding inertial sensor value, which are usually difficult to obtain and hard to change flexibly. To simulate the actual flight data, the automatic flight track generator is designed. The track generator is based on the great circle flight path control law, and takes the route turn mode and the random wind interference into consideration. Simulation results show that this method can simulate the actual flight status, so it has important reference value for verifying inertial navigation algorithm performance and optimizing the flight control law.