Research of Adaptive Dynamic Inversion method in Robust Fault Tolerant Flight control

The paper presents a design technique of robust controllers using Dynamic Inversion method and Model-Reference Adaptive Control with neural network control for longitudinal flight control.We use Dynamic Inversion to linearize the plant and decouple input-output,while neural network controller with improved PSO is designed to eliminate the disadvantage of Dynamic Inversion method that it's sensitive to the accurateness of models.The simulation results show that the adaptive robust flight control system has good dynamic qualities and the robustness ability.