Title :
Quantitative speed control for SRM drive using fuzzy adapted inverse model
Author :
Hwu, K.I. ; Liaw, C.M.
Author_Institution :
Dept. of Electr. Eng., Nat. Tsing Hua Univ., Hsinchu, Taiwan
fDate :
7/1/2002 12:00:00 AM
Abstract :
Quantitative and robust speed control for a switched reluctance motor (SRM) drive is considered to be rather difficult and challenging owing to its highly nonlinear dynamic behavior. A speed control scheme having two-degree-of-freedom (2DOF) structure is developed here to improve the speed dynamic response of an SRM drive. In the proposed control scheme, the feedback controller is quantitatively designed to meet the desired regulation control requirements first. Then a reference model and a command feedforward controller based on an inverse plant model are employed to yield the desired tracking response at nominal case. As the variations of system parameters and operating conditions occur, the prescribed control specifications may not be satisfied any more. To improve this, the inverse model is adaptively tuned by a fuzzy control scheme so that the model-following tracking error is significantly reduced. In addition, a simple disturbance cancellation robust controller is added to improve the tracking and regulation control performances further.
Keywords :
feedforward; fuzzy control; model reference adaptive control systems; reluctance motor drives; velocity control; SRM drive; command feedforward controller; control specifications; disturbance cancellation controller; fuzzy adapted inverse model; fuzzy control scheme; inverse plant model; model-following tracking error; nonlinear dynamic behavior; operating conditions; quantitative speed control; reference model; regulation control requirements; speed dynamic response; switched reluctance motor; system parameters; tracking response; two-degree-of-freedom structure; Fuzzy control; Integrated circuit modeling; Inverse problems; Reluctance machines; Reluctance motors; Robust control; Rotors; Torque; Transfer functions; Velocity control;
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
DOI :
10.1109/TAES.2002.1039411