Design of Disturbance Observer with Error Recursive Reduction Computational Technique for Aircraft System Using State Feedback with Integral Control Law
摘要
Closed loop control system research is extremely concentrated on attaining the feedback control system with minimum time domain specifications. In this paper, a new approach is proposed an error recursive reduction computational method (ERRC), to satisfy the needs of industries. The proposed method is applied with the Luenberger observer as a hybrid control system. The proposed method is highly focused on reducing closed loop system error in a rational way. A comparative analysis is performed with and without the error recursive reduction method in a Luenberger observer and is tested in Boeing’s commercial aircraft system and the efficiency of the proposed controller is evaluated on the basis of time domain specification, servo and disturbance rejection analysis. This method is proposed for industrial application, to minimize the error and the process reaction time.