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基于两路GPS信息接收和切换的无线信标机设计 被引量:1
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作者 郑俊华 谭秋林 秦小龙 《电子器件》 CAS 北大核心 2015年第4期863-867,共5页
通过对目前信标机的应用范围及国内外的发展状况进行研究,设计了一种基于两路GPS信息接收和切换的无线信标机。控制电路采用C8051F040单片机作为主控芯片,控制两路GPS模块的切换从而增加无线信标机的工作时间,提高定位精度并降低功耗。... 通过对目前信标机的应用范围及国内外的发展状况进行研究,设计了一种基于两路GPS信息接收和切换的无线信标机。控制电路采用C8051F040单片机作为主控芯片,控制两路GPS模块的切换从而增加无线信标机的工作时间,提高定位精度并降低功耗。实验测得UTC时间为11:37:30,北纬38.013 6°,东经112.446°,海拔高度为815.9 m。多次测量结果表明,该系统能实现定位数据的接收与转发并将定位信息通过上位机进行显示。 展开更多
关键词 电路与系统 信标机设计 无线通信 两路GPS定位 低功耗
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X频段信标机的设计与实现 被引量:2
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作者 梁盛 潘高峰 +1 位作者 薛军 谢勇 《电讯技术》 北大核心 2017年第9期1088-1091,共4页
为满足船载X频段测控设备信道相位修正和伺服性能检查的需要,设计并研制了一款X频段信标机。首先,选用HMC765LP6CE芯片,利用频率合成技术设计了信源并通过通用串行总线(USB)实现了发射频率用户自定义;其次,针对安装平台面积小的限制,基... 为满足船载X频段测控设备信道相位修正和伺服性能检查的需要,设计并研制了一款X频段信标机。首先,选用HMC765LP6CE芯片,利用频率合成技术设计了信源并通过通用串行总线(USB)实现了发射频率用户自定义;其次,针对安装平台面积小的限制,基于高频结构仿真器(HFSS)设计了高次模微带天线并完成了仿真分析和指标优化;最后,完成了X频段信标机的工程实现并给出了硬件电路结构和软件程序设计方法。经测试,该信标机锁相效果良好,控制简便,性能可靠,满足用户使用要求。 展开更多
关键词 X频段测控设备 信标机设计 直接频率合成 微带天线
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Determining the approach speed envelope of carrier aircraft 被引量:3
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作者 Geng Jianzhong Yao Hailin Duan Zhuoyi 《Engineering Sciences》 EI 2013年第6期19-23,31,共6页
Many factors,such as deck motion and air wave,influence the determination of the approach speed which has an important effect on landing safety. Until recently,there are no design criteria about approach speed of carr... Many factors,such as deck motion and air wave,influence the determination of the approach speed which has an important effect on landing safety. Until recently,there are no design criteria about approach speed of carrier aircraft in the current standards and available publications. Therefore,the requirements of stall margin, longitudinal acceleration ability,altitude correction and field-of-view on approach speed were researched. Based on the flight dynamics model,the flight simulations were conducted to study the effect of the response time of engine,wave off requirements,elevator efficiency and deflection rate on the approach speed. The results presented that the approach longitudinal acceleration and altitude correction ability had crucial influence on the approach speed envelope of the aircraft. The limitations of the control requirements,field- of- view requirements and gear were also given through the simulation and analysis. Based on the above results,the approach speed envelope were determined. 展开更多
关键词 carrier aircraft approach speed altitude correction handling quality landing safety
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