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本文研究了飞行训练用航空发动机转速模拟系统拟最少拍控制设计。采用电液泵控马达系统能满足航空发动机转速模拟系统对大功率的要求，但在大幅度阶跃输入下的动态响应难以达到预期的要求。本文提出的拟最少拍控制设计解决了这一问题，实验验证了设计的有效性。
This paper studies the aero-engine speed simulation system for flight training to simulate the minimum control design. The use of electro-hydraulic pump motor system can meet the requirements of aero-engine speed simulation system for high power, but it is difficult to meet the expected requirements under large step input dynamic response. The quasi-minimal control design proposed in this paper solves this problem and validates the validity of the design experimentally.