研究了一种模糊控制方法，并用于分级燃烧循环液体火箭发动机变工况过程的反馈控制。
A fuzzy control is studied, which is used for the feedback control in the changing condition process of the staged combustion cycle liquid rocket engine.
针对分级燃烧循环液体火箭发动机启动过程的特点，提出了一种变结构控制系统。
A variable structure control system for the start up process of staged combustion cycle liquid rocket engine is presented in this paper.
提出了一种新的液体火箭发动机分级燃烧循环最高室压计算方法。
A new modular method for calculating the maximum combustion chamber pressure with stage combustion cycles is proposed in this paper.
提出了一种新的液体火箭发动机分级燃烧循环最高室压计算方法。
A new modular method for calculating the maximum combustion chamber pressure with stage combustion cycles is proposed in this paper.
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