Ground, aviation integral autonomous navigation system design method

The invention discloses a ground-space-sky integrated autonomous navigation system design method, which is an autonomous navigation system design method that can be applied to the whole process of launching aircrafts from the ground to the deep space for detection. A system at least comprises a pseudo satellite, a pulsar, a ground main control station, an aircraft, etc. The system is combined with an on-orbit operating GPS or Chinese 'Beidou' satellite so as to be integrated into an autonomous navigation positioning system as a whole. The method prospectively fuses the pulsar which is a stable signal source still in physical concepts into the technical category of deep space integrated autonomous navigation. The method systematically solves the integration requirements of the autonomous navigation of deep space aircrafts, effectively realizes the information fusion of a variety of high technology application, and satisfies the high-precision autonomous navigation application of aircrafts in deep space detection activities. Meanwhile, the method is also a new exploration for the expanding study and system method of ground navigation positioning application.