A Study on Quick Cockpit for Flight Simulators Prototype Systems

被引：0

作者：

Liu Guangda ^{[1
]}

Huang Qitao ^{[1
]}

Zhang Bing ^{[1
]}

Han Junwei ^{[1
]}

Xu En-yong ^{[2
]}

机构：

[1] Harbin Inst Technol, Sch Mechatron Engn, Harbin 150006, Peoples R China

[2] Dongfeng Liuzhou Motor CO LTD, Technol Res Ctr, Liuzhou, Peoples R China

来源：

2009 INTERNATIONAL CONFERENCE ON MEASURING TECHNOLOGY AND MECHATRONICS AUTOMATION, VOL II | 2009年

关键词：

flight simulator; interface system; standard IO system; prototype systems CAN bus;

D O I：

10.1109/ICMTMA.2009.492

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

The development of flight simulator prototype systems is a challenging work because of its complexity. A common problem faced in the design of the flight simulator is how to build the cockpit. The cockpit contains thousands of data acquiring point, and very complex logics. Too much time wilt be spend on designing the board and debugging the code if the cockpit Data Acquire (DAQ) system is not well designed. This paper describes a kind of DAQ boards' suite and a software structure to make the work of building the cockpit easier. A standard IO system is showed in the paper construct by the DAQ system and Controller Area Network (CAN) bus which build for the flight simulators prototype systems. A detailed analysis about the data characteristics of panels Is given and a structure of DAQ board sets is discussed. A software framework is presented in the paper. Conclusions drawn from the experience of implementing the design are also given.

引用

页码：28 / +

页数：3

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