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舰载机不同弹射系统的弹射过程
引用本文:甄子洋,江驹,王新华,朱熠.舰载机不同弹射系统的弹射过程[J].电光与控制,2012,19(5):7-10.
作者姓名:甄子洋  江驹  王新华  朱熠
作者单位:南京航空航天大学自动化学院,南京,210016
基金项目:南京航空航天大学引进人才科研启动基金,南京航空航天大学基本科研业务费专项科研资助项目,航空科学基金
摘    要:针对目前世界上最典型的两种舰载机弹射系统:蒸汽弹射系统和电磁弹射系统,对比研究了不同弹射系统的结构原理、数学模型、弹射性能等问题。分析了常用的蒸汽弹射装置和电磁装置的组成部件及其功用,给出对比分析结果;根据蒸汽弹射装置和电磁弹射装置的运动学特性,获得两种弹射装置的数学模型,推导出它们的非线性运动学方程,并给出对比分析结果;针对两种不同的弹射系统,构建了舰载机在舰面加速段的弹射过程的Matlab数值仿真模型,通过仿真研究,分析了不同弹射系统中对弹射性能起主要影响作用的关键因素,并根据仿真结果进行了对比分析。

关 键 词:舰载机  弹射起飞  蒸汽弹射  电磁飞机弹射系统
收稿时间:2011/5/16

Catapult Process of Different Catapult Systems for Carrier-Based Aircraft
ZHEN Ziyang , JIANG Ju , WANG Xinhua , ZHU Yi.Catapult Process of Different Catapult Systems for Carrier-Based Aircraft[J].Electronics Optics & Control,2012,19(5):7-10.
Authors:ZHEN Ziyang  JIANG Ju  WANG Xinhua  ZHU Yi
Affiliation:(College of Automation Engineering, Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China)
Abstract:The structureprinciplemathematical models and performance were studied for the two typical methodssteam catapult and Electromagnetic Aircraft Launch System(EMALS)for catapult launch of carrier based aircraft.The compositions of steam catapult and EMALS were analyzed.The functions of the different parts of the catapult systems were also discussed.According to the kinematical characteristics of steam catapult and EMALSthe mathematical models were establishedtheir nonlinear kinematical equations were deduced and the comparative analysis reslult was given.Simulations were made for the two catapult methods on the speeding stage of the aircraft.The main factors that have effect on catapult launch performance were analysed for different catapult methods by using the simulation result.Comparison of the two catapult launch systems was also made.
Keywords:carrier based aircraft  catapult launch  steam catapult  electromagnetic aircraft launch system
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