冲压发动机控制建模及多变量控制系统变换研究

Huafeng Yu, Yingqing Guo, Xinghui Yan, Jiamei Wang
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引用次数: 0

摘要

随着飞行马赫数的增加,冲压发动机已成为一种理想的动力。由于实验成本的上升和实验难度的增大,有必要在系统的初始阶段建立数字仿真模型。首先,给出了考虑进气道激波系统位置和执行机构动力学的准一维构件模型建立方法;通过构造通用工作方程,实现了进气道的部件匹配和起动裕度的计算。然后,根据现有的单变量控制系统,设计了多变量控制系统的改造方案,采用鲁棒保成本控制方法实现了多变量控制器的设计。最后,通过对冲压发动机和控制系统的仿真,表明在推力响应基本相同的情况下,变换后的多变量控制器可以提高进气道的启动裕度,提高发动机的安全性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Research on Ramjet Modeling for Control and Multivariable Control System Transform
With the increase of flight Mach number, ramjet has become an ideal power. Due to the rising cost and difficulty of experiments, it is necessary to establish a digital simulation model in the initial stage of the system. First, a quasi-one-dimensional component model establishment method is given, which takes the position of the inlet shock wave system and the dynamics of the actuator into account. The component matching and the calculation of the starting margin of the inlet are realized by constructing a common working equation. Then, according to the existing single-variable control system, a multi-variable control system transformation scheme is designed, and the multi-variable controller design is realized by using the robust guaranteed cost control method. Finally, through the simulation of the ramjet engine and control system, it is shown that the transformed multivariable controller can improve the starting margin of the inlet and increase the safety of the engine under the condition that the thrust response is basically the same.
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