机构

• 国家空间科学中心 [5]
• 长春光学精密机械与物... [1]

采集方式

• OAI收割 [6]

内容类型

• 会议论文 [4]
• 期刊论文 [2]

发表日期

• 2014 [2]
• 2013 [3]
• 2010 [1]

学科主题

• 空间技术 [3]

筛选

浏览/检索结果: 共6条，第1-6条 帮助 条数/页： 5101520253035404550556065707580859095100 排序方式： 请选择题名升序题名降序提交时间升序提交时间降序作者升序作者降序发表日期升序发表日期降序 1553B总线与RS485总线通信转接系统的设计 期刊论文  OAI收割 微电子学与计算机, 2014, 卷号: 31, 期号: 3, 页码: 1-4 作者:  周莉;  安军社 收藏  |  浏览/下载：39/0  |  提交时间：2015/09/22 网关  桥接器  1553B总线  RS485总线   1553B总线与 RS485总线通信转接系统的设计 期刊论文  OAI收割 微电子学与计算机, 2014, 卷号: 31, 期号: 3, 页码: 1-4 周莉,安军社 收藏  |  浏览/下载：54/0  |  提交时间：2014/07/14 网关  桥接器  1553B总线  RS485总线  FPGA   Design of a RS485-to-1553B Bus Bridge 会议论文  OAI收割 5th International Conference on Cyber-Enabled Distributed Computing and Knowledge Discovery (CyberC), Beijing, PEOPLES R CHINA, OCT 10-12, 2013 作者:  Zhou, Li;  An, Junshe 收藏  |  浏览/下载：51/0  |  提交时间：2014/04/30 RS485  1553B bus  FPGA  bridge  aerospace application   Study on the low power technologies of 1553B bus 会议论文  OAI收割 2013 IEEE International Conference on Signal Processing, Communications and Computing, ICSPCC 2013, Kunming, Yunnan, China, August 5, 2013 - August 8, 2013 作者:  Zhou, Li;  An, Junshe 收藏  |  浏览/下载：32/0  |  提交时间：2014/04/30 Low power  MIL-STD-1553B  IP core  RS485 bus  Infrared communication.   Design of a Payload Data Handling System for Satellites 会议论文  OAI收割 3rd International Conference on Instrumentation & Measurement, Computer, Communication and Control (IMCCC), Shenyang, PEOPLES R CHINA, SEP 21-23, 2013 作者:  Zhou, Li;  An, Junshe 收藏  |  浏览/下载：21/0  |  提交时间：2015/10/26 onboard data handling  payload data handling system  1553B bus  RS485  onboard computer   Small aircraft CAN bus signal acquisition equipment (EI CONFERENCE) 会议论文  OAI收割 2010 International Conference on Computer, Mechatronics, Control and Electronic Engineering, CMCE 2010, August 24, 2010 - August 26, 2010, Changchun, China Chen C.-Q. 收藏  |  浏览/下载：29/0  |  提交时间：2013/03/25 Small aircraft often used RS485 bus. But with the complexity of the small aircraft's subsystems increase and the progress of field bus technology  CAN bus systems in small aircraft use more and more widely. How to record real-time flight experiment data on the small aircraft's CAN bus and provide test data for reproducing the process of a small aircraft flying is very important. This paper presents a design method of signal acquisition device  it can be used for small aircraft flying field experiment. 2010 IEEE.  as the main chip with DSP2812  SJA1000 as CAN controller  CTM1050 as the CAN transceiver  CF card as storage media. Gives the diagram of its hardware and software design process. Combined with the background of a small aircraft  testing the instrument for data acquisition when the ground experiments and flight progress. Experimental data show that the design of high reliability and CAN signals can effectively complete the record