首页 | 本学科首页   官方微博 | 高级检索  
     

双余度飞行显示控制计算机的设计与实现
引用本文:左清清,梁争争,王斌,赵楠. 双余度飞行显示控制计算机的设计与实现[J]. 电子技术, 2014, 0(9): 81-83
作者姓名:左清清  梁争争  王斌  赵楠
作者单位:中国航空计算技术研究所,陕西 西安
摘    要:飞行显示控制计算机是飞行员高效、直观地获取所需信息或发送控制命令的操作平台,其任务可靠性对飞机飞行安全至关重要,一旦失效将会造成系统部分或全部功能丧失,尽管不会直接危及飞行员人机安全,但会严重影响飞行和作战任务的完成。因而本设计采用了双余度设计方法,有效提高了任务可靠性、降低了失效风险,具备一定的工程实用价值。

关 键 词:飞行显示控制计算机  任务可靠性  双余度

Design and Implementation of Flight Display Control Computer with Dual Redundancy
Zuo Qingqing,Liang Zhengzheng,Wang Bin,Zhao Nan. Design and Implementation of Flight Display Control Computer with Dual Redundancy[J]. Electronic Technology, 2014, 0(9): 81-83
Authors:Zuo Qingqing  Liang Zhengzheng  Wang Bin  Zhao Nan
Affiliation:Zuo Qingqing Liang Zhengzheng Wang Bin Zhao Nan (Aeronautical Computing Technique Research Institute, AVIC, Xi'an, Shaanxi)
Abstract:Flight display control computer is an operation platform for pilots to obtain necessary information and send control command efficiently and intuitionally. Its mission reliability is critical and essential to aircraft's flight safety. Once it is failed part or all of system functions will lose, and although this will not endanger the life of pilots, but will influence flying and the completion of battle mission seriously. Consequently, this design adopts dual redundancy method, effectively improving the mission reliability, reducing the failure risk, and has a certain practical value.
Keywords:flight display control computer  mission reliability  dual redundancy
本文献已被 CNKI 维普 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