Optimum performance seeking control of aero-engine based on Sequential Quadratic Programming

A methodology based on the nonlinear algorithm of Sequential Quadratic Programming in engine performance seeking control is presented. This article is aimed at analyzing the inherent limitation and max-acceleration. Simulation result shows that the engine has better acceleration performance through seeking control, and Sequential Quadratic Programming is suitable for the Optimum performance seeking control of engine, and SQP is suitable for the optimum performance seeking of engine.