Analysis of Home LED Intelligent Lighting Interoperation

来源 :第十二届中国国际半导体照明论坛 | 被引量 : 0次 | 上传用户:a6231423
下载到本地 , 更方便阅读
声明 : 本文档内容版权归属内容提供方 , 如果您对本文有版权争议 , 可与客服联系进行内容授权或下架
论文部分内容阅读
  Three different LED intelligent lighting architectures are analyzed and four interoperability support elements are extracted.Three levels of lighting interoperation modes that can be utilized in LED intelligent lighting system are discussed based on these elements and the characteristics of lighting interoperation modes are compared under the criteria of real-time performance,reliability and scalability.Suitable scenarios for each mode are obtained,that is helpful for promoting the formulation of unique intelligent lighting standards and more LED intelligent lighting products can be developed to meet consumers demands.
其他文献
随着时间频率标准研究的飞速发展,理论不确定度水平在10-16-10-18的喷泉钟和光钟先后成为现实,如何将这种高准确度的时间频率低损耗的传输出去成了急待解决的问题.基于光纤的标准时间频率信号传输技术提供了一个可行的方案.光纤本身具有体积小、重量轻、不受电磁辐射影响、埋入地下受温度和应力的影响小等优点,可以通过伺服补偿光纤传输过程中的噪声干扰,实现标准频率信号传输路径的稳定.本文基于远距离实际光纤链
在动态精密单点定位中,多GNSS组合PPP与PPP模糊度固定技术都具有提升定位性能的作用.本文联合使用以上两种技术,实现了BDS辅助下的GPS PPP模糊度固定,并利用MGEX测站的数据进行GPS浮点解、GPS固定解、BDS/GPS浮点解、BDS/GPS固定解四种PPP动态实验,结果表明:在观测时长为4h的情况下,GPS PPP模糊度首次固定时间(TTFF)约为48.3分钟,模糊度固定率为74.4
地球静止轨道(GEO)卫星由于独特的高轨和静地特性,在通信、气象、侦察、导航定位、授时、跟踪与数据中继以及科学研究等方面发挥着越来越重要的作用,地球静止轨道卫星的自主定轨技术已经成为我国迫切需要发展的航天新技术之一.针对利用星地观测数据对GEO卫星实现定轨存在观测几何差的问题,本文提出了一种基于优化PDOP值星间链路的GEO卫星自主定轨方法.首先,基于建立的仿真场景分析了MEO卫星与GEO卫星所建
For the sake of steadily tracking carrier signal under high dynamic or low C/N0 (Carrier to Noise Power Ratio) environments,during various tracking loop structure of GNSS (Global Navigation Satellite
Indoor location based servicedemandsprecisevertical height information and its degree of distinguishing in the vertical position should be decimeter,so that we can precisely recognize the building flo
Pulse navigation signal is usually utilized to carry navigation in-formation instead of continuous signal by pseudolite navigation systems such as LOCATA,whose carrier tracking methods commonly use tr
The aerospace TT&C system plays an important role in tracking space-craft,and it is necessary for maintaining its good performance and precision.This paper focuses on the application of BDS in the pre
Earth Orientation Parameters (EOP) is essential for spacecraft navigation missions,such as deep space navigation and GNSS navigation mission,directly affecting navigation accuracy of spacecraft.Firstl
In this paper,a high-performance compact rubidium frequency standard (CRFS) has been successfully developed,of which the frequency stability (Allan variance) reached 3E-12/τ0.5(τ=1s~1000s) and frequen
Based on the correlation coefficient between the time series of the GPS network,extracting the common mode error(CME) using principal component analysis(PCA) in Crustal Movement Observation Network of