In project proposes, a neural tuning technique is proposed and applied to a Fractional Order Proportional Integral Derivative (FOPID) controller. The proposed controller is applied to a radar guided missile which is used for tracking high speed moving targets in defense systems. The proposed neural tuning along with H2/H∞ optimization method is intended to improve the tracking performance of the Proportional Navigation (PN) system and the stability of the missile trajectory during flight time. Due to the coupled and nonlinear dynamics of the considered missile, we propose a new control structure that integrates the fractional order PID controller into the proportional navigation system of the missile which results in better stability properties for the missile. In order to tune the FOPID we proposed a neural tuning technique that starts with a genetic algorithm based optimizer and continues with a neural network based scheme. This speeds up finding a near optimal solution and refining it effectively. Then, H2/H∞ optimization process is applied within the neural tuning technique to achieve better stability and tracking performance for the missile during the whole flight time. The proposed controller is compared with the standard PID controller tuned by the conventional Ziegler–Nichols (ZN) tuning method as well as Particle Swarm Optimization (PSO) method and the simulation results proved the superiority of the proposed tuning method over ZN and PSO based tuning approaches.

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