DocumentCode
3019347
Title
Design of comprehensive general support system for airborne inertial platform
Author
Xu Li ; Ye Zhan ; LiMin Chang ; Yan Zang
Author_Institution
Flight Vehicle Control Dept., Aviation Univ. of Air Force, Changchun, China
fYear
2013
fDate
20-22 Dec. 2013
Firstpage
223
Lastpage
226
Abstract
Aiming at the problems of guarantee equipment deficiency and poor versatility in airborne inertial platform system, and adopting ATE design ideas, this paper presents a design scheme of comprehensive general support system based on PXI bus architecture. Putting forward the classified switching technology, hardware resources are made of reasonable extension, thus it realizes the integrated support of platform of INS and SINS. Adopting the virtual technology, software architecture of support platform are hierarchical, modular and interface. Thus, it realizes the integrated control of test system. Adopting improved generalized likelihood ratio method reduces the system undetected rate and false alarm rate. The practice has proved that this support platform has the advantage of stable operation, good versatility, strong practicality and broad application prospects.
Keywords
aircraft navigation; control engineering computing; inertial navigation; software architecture; PXI bus architecture; airborne inertial platform; classified switching technology; comprehensive general support system design; generalized likelihood ratio method; hardware resources; inertial navigation systems; software architecture; test system integrated control; Hardware; Inertial navigation; Military aircraft; Reliability; Resource management; Software; Switches; Airborne Inertial Platform; Classified switching; PXI Bus; Virtual System;
fLanguage
English
Publisher
ieee
Conference_Titel
Mechatronic Sciences, Electric Engineering and Computer (MEC), Proceedings 2013 International Conference on
Conference_Location
Shengyang
Print_ISBN
978-1-4799-2564-3
Type
conf
DOI
10.1109/MEC.2013.6885076
Filename
6885076
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