高超声速发动机分布参数控制问题

Distributed Parameter Control method for Hypersonic Jets

高超声速发动机表现出了明显的分布参数特性,采用集中参数控制方法难以满足发动机控制要求。本文结合分布参数控制理论的研究进展和周边的学科的发展,提出了高超声速发动机分布参数控制问题,是对传统的集中参数控制构架的继承和突破。分布参数控制体系的新原理、方法、实现手段将对高超声速发动机系统的运行和设计产生重要影响。

Hypersonic jets show obvious distributed parameter characteristics, and the concentrated parameter control method is hard to function. In this paper, the distributed parameter control method for hypersonic jets which was the succession and breakthrough of traditional concentrated parameter control method was put forward after analyzing the development of distributed parameter control theory and corresponding circumjacent subjects. The new principles and methods of distributed parameter control may have an impact on the operation and design of hypersonic jets.