Design method of an intelligent pilot for missiles under space constraint

In order to change the long design cycle and poor generalization of the classical control-based missile autopilot designed, and the lack of control capability in the face of large angle-of-attack changes and complex aerodynamic changes, the missile smart pilot under spatial constraints is designed, and experiments on the missile smart pilot tracking time-varying and time-invariant signals and flight pull-off control experiments are carried out under a Python-based simulation platform. The experiments show that the missile smart pilot is able to track the specified signal quickly, and its average tracking effect is 26.4% faster, 18.1% more accurate, and 17.6% more stable than the classical control law. And the convergence of the smart pilot is verified by four algorithms and a variety of simulation beats, showing that the smart pilot design cycle can be shortened by the design of the completed control law. Through simulation comparison verification, the smart driver can achieve stable accurate and fast tracking.