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讨论了一种具有飞行与推力综合系统的舰载机自动着舰控制系统的设计方法。结合国产某型飞机，首先分析了基于俯仰姿态的升降速率控制系统的结构与控制规律；然后，对飞机进场功率补偿系统的结构与控制规律进行了分析；最后，在同时考虑飞行控制系统与发动机推力补偿控制系统的条件下，对该综合系统的控制规律进行了设计与仿真，并提供了仿真结果。
The design method of the automatic landing control system of carrier-based aircraft with integrated flight and thrust system is discussed. Combined with a domestic aircraft, the structure and control law of the lift-and-descent rate control system based on pitch attitude are analyzed first. Then the structure and control law of the aircraft power compensation system are analyzed. Finally, considering both the flight control system and Engine thrust compensation control system under the conditions of the control system of the integrated system design and simulation, and provide simulation results.