Research on Control Algorithm Design for Aero-Engine Vane Angle on Dynamic Process

摘要

This paper investigates the control law of aero-enginevane angle on dynamic process. Two kinds of corrected algorithm is presented to solve the problem of large pertur bation of vane angle at the end of dynamic process. The problem is solved by using the m ethod of slope restri ction on perturbation and reducing the am plitude of the perturbation. The effectness of two methods is validated by simulation, and simulation results show that the presented algorithm can be used both individually and associatively. By using these methods, the perturbation of vane angle on dynamic process can be reduced, andaccordingly, the stability influence of engine in transition process is ensured better.