首页 | 本学科首页   官方微博 | 高级检索  
     

飞机全电刹车驱动器设计与关键技术研究
引用本文:刘冠志,林辉. 飞机全电刹车驱动器设计与关键技术研究[J]. 计算机测量与控制, 2010, 18(2)
作者姓名:刘冠志  林辉
作者单位:西北工业大学,陕西西安,710072
基金项目:航空科学基金项目(2007ZC53036)
摘    要:为提高全电刹车系统驱动器的静态、动态性能和可靠性,提高刹车系统的执行能力,针对系统中的关键技术进行了研究,在充分发挥DSP与CPLD功能的基础上,提出了合理的控制策略、软件设计和硬件设计,并对影响电路可靠性的因素进行了分析,提出了解决方案;在不同的工作状态下进行了试验,检验了驱动器的各项性能;试验结果表明,该设计性能优良,能够满足全电刹车系统的要求。

关 键 词:全电刹车  DSP  CPLD  中断  分段PID  

Design of Drive in Aircraft Electric Brake System and Research on Key Technology
Liu Guanzhi,Lin HUi. Design of Drive in Aircraft Electric Brake System and Research on Key Technology[J]. Computer Measurement & Control, 2010, 18(2)
Authors:Liu Guanzhi  Lin HUi
Affiliation:Northwestern Polytechnical University/a>;Xi'an 710072/a>;China
Abstract:In order to improve the static and dynamic performance and the reliability of the drive which is in the electric brake system to enhance the system's implementation capacity,key technology of the drive have been studied.Taking full advantage of the function of DS Pand CPLD,the paper gives reasonable control strategy,software design and hardware design and puts forward solutions for the factors which affect the circuit reliability.The performance of the drive has been tested in different conditions and exper...
Keywords:electric brake  DSP  CPLD  interruption  sub-PID  
本文献已被 CNKI 万方数据 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号