舰载机动力补偿系统设计

Design of power compensation system for shipborne aircraft

大型军事舰船,特别是具有战斗机运载能力的舰船(航空母舰等)是一个国家非常重要的战略力量,对保卫国家海上领土有重要意义。舰载机是指以航空母舰等为基地的飞行器统称,按照机翼结构可以分为固定翼飞机和直升机等形式。舰载机的起飞与降落问题一直是军事领域的重点和难点,本文的研究对象是舰载机在着舰时的动力补偿系统,该系统的主要作用是保证飞机器在着舰时具有合理的速度和加速度,保持稳定、安全的着舰。本文首先介绍了舰载机动力补偿系统的原理,然后在舰载飞机的动力学模型的基础上,设计了一种基于PID控制的舰载飞机动力补偿系统。

Large military ships, especially those with the carrying capacity of fighter planes(aircraft carriers, etc.), are a very important strategic force of a country and are of great significance to the defense of the country’s maritime territory.Shipborne aircraft refers to aircraft based on aircraft carriers and so on. According to the wing structure, it can be divided into fixed-wing aircraft and helicopter. The take-off and landing of carrier-based aircraft has always been the focus and difficulty in the military field. The research object of this paper is the dynamic compensation system of carrier-based aircraft when landing. The main function of this system is to ensure that the aircraft has reasonable speed and acceleration when landing, and maintain stable and safe landing. Firstly, the principle of power compensation system for shipborne aircraft is introduced. Then, based on the dynamic model of Shipborne aircraft, a power compensation system for shipborne aircraft based on PID control is designed.