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In order to shorten the displacement during missile flight and achieve the purpose of accurate cruise positioning, a cruise missile controller based on the optimal control law of LQR is designed. According to the supply demand of the missile power circuit, PID control elements, cruise actuators, longitudinal missile catapults and range regulators are connected to build the main structural unit of the cruise missile controller. According to the initialization standard of the control module, the fuzzy control of the control coefficients is realized, and then the cruise rule base is combined to calculate the actual optimization effect of the LQR control coefficients, complete the cruise model controller sensitivity analysis based on the LQR optimal control law, and realize cruise missile control Smooth application. The comparative experimental results show that compared with ordinary component control equipment, after applying the new controller equipment designed by the subject, the missile flight displacement is reduced from 93000Km to about 60,000Km, and the UDA dominance coefficient also exceeds 1.0, which can solve the missile cruise positioning accuracy not meeting the standards The problem.