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基于序列二次规划算法的发动机性能寻优控制
引用本文:孙丰诚,孙健国.基于序列二次规划算法的发动机性能寻优控制[J].航空动力学报,2005,20(5):862-867.
作者姓名:孙丰诚  孙健国
作者单位:南京航空航天大学,能源与动力学院,江苏,南京,210016
基金项目:航空科学基金资助(04C52019)
摘    要:提出用非线性序列二次规划(SQP,Sequen tial Q uadratic P rogramm ing)算法解决发动机性能寻优控制问题。分析了线性规划(LP,L inear P rogramm ing)算法用于发动机性能寻优的固有缺陷以及SQP算法的优点。给出了SQP算法与LP算法用于最大推力模式和最小油耗模式仿真结果对比曲线。数字仿真实验的结果表明,SQP算法具有比LP算法更好的优化效果,在工程实际中有很大的应用潜力。

关 键 词:航空、航天推进系统  序列二次规划  线性规划  涡扇发动机  性能优化  最大推力模式  最小油耗模式
文章编号:1000-8055(2005)05-0862-06
修稿时间:2004年10月24

Aero-Engine Performance Seeking Control Based on Sequential Quadratic Programming Algorithm
SUN Feng-cheng,SUN Jian-guo.Aero-Engine Performance Seeking Control Based on Sequential Quadratic Programming Algorithm[J].Journal of Aerospace Power,2005,20(5):862-867.
Authors:SUN Feng-cheng  SUN Jian-guo
Abstract:A methodology based on the nonlinear algorithm of Sequential Quadratic Programming(SQP) in aero-engine performance seeking control was presented.This article is aimed at analyzing the inherent limitation of Linear Programming used for aero-engine performance seeking control and to solve the problem of aero-engine performance optimization using nonlinear SQP method.The results of numerical simulations of maximum thrust mode and minimum fuel consumption mode using SQP and LP respectively show that SQP algorithm has better optimization result than LP algorithm.SQP algorithm has great application potential in engineering.
Keywords:aerospace propulsion system  Sequential Quadratic Programming(SQP) algorithm  Linear Programming(LP) algorithm  turbofan engine  performance optimization  maximum thrust mode  minimum fuel consumption mode
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