Research of Integrative GNC Design Simulation for Cruise Missile

Scheme guidance is widely used in the gaining altitude phase and level flight phase of cruise missile. The missile aviates according to the planed procedure, but the unchanged scheme can´t adapt to the large diversification which will possibly occur in flight, and will result in a long time´ response. This paper brings forward a design method of integrative GNC, which combines the navigation information with the scheme component. In certain conditions, the scheme component will start up flexible flight procedure, meanwhile transfer the manipulative parameters into the ones which are fit the real-time situation, and end in the smooth transition between scheduled aim and provisional flight path.