首页 | 本学科首页   官方微博 | 高级检索  
     

基于磁流变液的飞机起落架嵌入式缓冲控制器设计
引用本文:傅莉,李彬彬,胡为,陈新禹. 基于磁流变液的飞机起落架嵌入式缓冲控制器设计[J]. 火力与指挥控制, 2016, 0(9): 128-131. DOI: 10.3969/j.issn.1002-0640.2016.09.029
作者姓名:傅莉  李彬彬  胡为  陈新禹
作者单位:1. 沈阳航空航天大学航空航天工程学部,沈阳,110136;2. 沈阳航空航天大学自动化学院,沈阳,110136
基金项目:国家自然科学基金(61074090);中航创新基金(cxy2013SH16);辽宁省自然科学基金联合资助项目(2015020061)
摘    要:基于飞机着陆和滑行过程中,飞机起落架中磁流变阻尼器的阻尼力的不可控的问题。提出基于磁流变液的飞机起落架嵌入式缓冲控制器设计方法,设计了针对控制磁流变阻尼器阻尼力的缓冲控制系统,主要包括嵌入式数字信号处理器DSP的选择,控制系统的原理设计,电源产生电路和复位电路模块,JTAG仿真电路模块,A/D采样校正模块,D/A转换模块,压控电流源驱动模块。通过电路模块的仿真,由控制系统中压控电流源出来的电流在阻尼器接受范围之内,证明了设计的磁流变缓冲控制器能对阻尼力的大小进行控制,对飞机起落架的缓冲系统起到调节作用。

关 键 词:飞机起落架  阻尼力  嵌入式  缓冲控制器  数字信号处理器

Aircraft Landing Gear Embedded Buffer Controller Design Based on Magneto-rheological Fluid
Abstract:Based on problem that the magneto rheological damper damping force of aircraft landing gear is not controllable in the process of aircraft landing and taxiing. A method of embedded buffer controller of aircraft landing gear based on magneto rheological fluid is presented and buffer control system is designed to control the magneto rheological damper damping force,which mainly includes the selection of embedded digital signal processor (DSP)and the principle design of control system,power generation and reset circuit modules,JTAG emulation circuit module,A/D sampling correction module, D/A converter module,voltage controlled current source driver module. Through the simulation of circuit module,the current in the magneto rheological buffer controller is accepted by the control system, the magneto rheological buffer controller designed can control damping force and play a regulatory role in the aircraft landing gear.
Keywords:aircraft landing gear  damping force  embedded  buffer controller  digital signal processor (DSP)
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