A Study of Novel Optimization Control for Aero Engine
A novel approach of optimization control based on Sequential Quadratic Programming (SQP) is suggested for aero engine. It is a global optimal method. There are two phases in every optimal step, termed long course optimization and short course optimization respectively. The objective functions were restructured based on long course optimization. And the short course optimization was carried out to correct the result. The optimal result was used for engine control. Aero engine acceleration control was simulated with using the globe optimization. The result indicated that the approach can solve the problem like the system with pure delay part and unmatched model which the general local optimization can not.
aero engine long course optimization short course optimization globe optimization
Zhao Lin Fan Ding
School of Engine and Energy, Northwestern Polytechnical University, Xian 710072, China
国际会议
2009 International Workshop on Information Security and Application(2009 信息安全与应用国际研讨会)
青岛
英文
345-348
2009-11-21（万方平台首次上网日期，不代表论文的发表时间）