摘要
根据电磁理论对舰载机起飞和降落过程进行建模分析,结合受控电压源模拟对电感线圈电流进行控制,根据受力建模分析得到了电流随时间的变化关系,作为后续闭环综合电磁装置控制系统的给定信号。针对舰载机质量和初始速度的改变对电磁装置参数进行灵敏性分析。探究保证舰载机可靠完成降落以及起飞过程的约束条件,同时考虑到在多种复杂情况下舰载机依然可以可靠起飞和降落,建立了闭环综合电磁装置控制系统,增强了系统的抗干扰能力。
Based on the electromagnetic theory,this paper models and analyzes the takeoff and landing process of the carrier aircraft.Combined with the controlled voltage source simulation,the current of the inductor is controlled.According to the force modeling analysis,the current changes with time are obtained,which can be used as the follow-up closed loop synthesis.The given signal of the electromagnetic device control system,and the sensitivity analysis of the parameters of the electromagnetic device for the change of the quality of the carrier aircraft and the initial speed are exploredto ensure the reliable completion of the landing and take-off process of the carrier aircraft.Takingallcomplex conditions into account,the carrier aircraft can still take off and land reliably.Aclosed-loop integrated electromagnetic device control system is established to enhance the anti-interference ability of the system.
作者
许允之
王仁顺
张可馨
XU Yunzhi;WANG Renshun;ZHANG Kexin(School of Electrical and Power Engineering,China University of Mining and Technology,Xuzhou 221116,Jiangsu,China)
出处
《实验室研究与探索》
CAS
北大核心
2020年第7期58-63,共6页
Research and Exploration In Laboratory
关键词
舰载机
电磁理论
电磁兼容
起飞降落
闭环系统
carrier aircraft
electromagnetic theory
electromagnetic compatibility
take off and landing
closed-loop system
