DocumentCode
682215
Title
Design and implementation of massive test metrical information management system in static structural test of aircraft
Author
Zuo Jia ; Zhang Jianfeng ; He Qian
Author_Institution
Full scale Aircraft Static/Fatigue Struct. Aviation Sci. & Technol. Key Lab., Aircraft Strength Res. Inst. of China, Xi´an, China
Volume
1
fYear
2013
fDate
16-19 Aug. 2013
Firstpage
183
Lastpage
186
Abstract
A massive test metrical information management system was designed and implemented, against the characteristic of massive test metrical information and the present status of lack of governing. The development platform for the system is Delphi 7.0, which is combined with Microsoft SQL Server 2000 database, and the Client/Server (c/s) structure was applied. In order to implement all functions of the system, firstly, function requirements analysis and division of functional module were performed; and then database modeling was executed; finally, the database structure and their applications were designed. The application of the system in practice proves that management system is an effective, accurate and convenient tool for mass test information management and processing, with which the productivity effect can be significantly improved.
Keywords
SQL; aircraft testing; automatic test software; client-server systems; database management systems; forecasting theory; information management; Client/Server structure; Delphi 7.0; Microsoft SQL Server 2000 database; aircraft; massive test metrical information management system; static structural test; Aerospace electronics; Aircraft; Conferences; Databases; Information management; Servers; Strain; Database; Delphi; Management system; Massive metrical information;
fLanguage
English
Publisher
ieee
Conference_Titel
Electronic Measurement & Instruments (ICEMI), 2013 IEEE 11th International Conference on
Conference_Location
Harbin
Print_ISBN
978-1-4799-0757-1
Type
conf
DOI
10.1109/ICEMI.2013.6743057
Filename
6743057
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