Predictive Adaptive Autopilot for STT Missile Based on Model Reference Method and Lyapanov Theorem

Due to different flight conditions, variation in mass-inertia characteristics, aerodynamic coefficients, disturbance and etc, dynamic equations are unknown and uncertain. therefore use of adaptive or robust control method for designing of autopilot which is related to unknown parameters variation in missile dynamic, autopilot parameters are variant,It cause this method to be necessary. In this paper first of all a predictive control is designed based on nonlinear model (NMPC) and tailor expansion and then by help of neural network in approximation of unknown functions in missile dynamic an model-reference predictive adaptive control is proposed for STT missile.