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对飞机纵向自动着舰控制系统进行了分析与研究。作者将升降速率（Ｈ－Ｄｏｔ）控制系统与进场推力补偿系统结合在一起，以便对飞行姿态和发动机的推力进行综合控制。文中讨论了该综合控制系统的控制规律、导引控制规律的设计方法以及舰体运动补偿网络及参数的选择方法。在考虑自由大气干扰、舰尾流和甲板运动的条件下，以国产某型号飞机为例，对其纵向自动着舰控制系统进行了分析、设计与仿真，并提供了部分仿真结果。
The aircraft longitudinal automatic landing control system was analyzed and studied. The author combines a H-Dot control system with an approach thrust compensation system to provide comprehensive control over flight attitude and engine thrust. The control law of the integrated control system, the design method of guidance control law and the selection method of hull motion compensation network and parameters are discussed in this paper. Under the condition of free air disturbance, ship wake and deck movement, taking a domestic model aircraft as an example, the vertical automatic landing control system is analyzed, designed and simulated, and some simulation results are provided.