摘要
本文主要介绍发动机过渡态控制系统分析时所必须的动态数学模型中应用的Broyden法解非线性方程组的方法。对Broyden法的程序实现也作了一定的介绍。
This paper mainly introduces the method of Broyden that is used to solve the unlinear equation group and this method, originally happlied in dynamic mathematical model, is necessary for the analysis of the aero engine's transition state control system. And also, this paper gives an introduction to the realization of the Broyder method's program.
出处
《长沙航空职业技术学院学报》
2002年第3期39-42,共4页
Journal of Changsha Aeronautical Vocational and Technical College
