The handing characteristics degradation of Carrier-based Aircraft in the Low-speed high angle of attack situation and the interference of the airflow disturbance can cause that Carrier-based Aircraft carrier landing failed if the Carrier-based Aircraft cannot be controlled well. This article focuses on building a carrier-based aircraft landing dynamics model that consider height affect, and analysis of the physical mechanism of carrier-based aircraft landing process. Designed Fuzzy PID control system for different Control channel, through comparative and analysis, draw their strength and weaknesses. Filter out the throttle lever height feedback PID controller as a control system under the airflow disturbance. Simulation results verify the effectiveness of the controller.