DocumentCode
497383
Title
A Study on Quick Cockpit for Flight Simulators Prototype Systems
Author
Liu Guangda ; Huang Qitao ; Zhang Bing ; Han JunWei ; Xu En-yong
Author_Institution
Sch. of Mechatron. Eng., Harbin Inst. of Technol., Harbin, China
Volume
2
fYear
2009
fDate
11-12 April 2009
Firstpage
28
Lastpage
31
Abstract
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 will 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 boardspsila 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.
Keywords
aerospace simulation; aircraft displays; controller area networks; data acquisition; prototypes; cockpit data acquire system; controller area network bus; data acquiring point; flight simulator prototype system; Aerospace engineering; Aerospace simulation; Costs; Data acquisition; Electric variables; Logic; Mechatronics; Prototypes; Software prototyping; Virtual prototyping; CAN bus; flight simulator; interface system; prototype systems; standard IO system;
fLanguage
English
Publisher
ieee
Conference_Titel
Measuring Technology and Mechatronics Automation, 2009. ICMTMA '09. International Conference on
Conference_Location
Zhangjiajie, Hunan
Print_ISBN
978-0-7695-3583-8
Type
conf
DOI
10.1109/ICMTMA.2009.492
Filename
5203370
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