DocumentCode
1738583
Title
Software reliability prediction of digital fly control system
Author
Shaoping, Wang ; Jianfrng, Tao ; Deliang, Kong
Author_Institution
Beijing Univ. of Aeronaut. & Astronaut., China
Volume
1
fYear
2000
fDate
2000
Abstract
With the rapid development of computer technology, software plays an important and decision-making role in the computer control system, especially in digital flight control systems. How to determine and improve the reliability of software is a critical problem demanding urgent solution. Traditionally, software reliability is determined according to a reliability model based on software testing data after the software has developed, which is not suitable for improving its reliability. This paper studies a method to predict the software reliability in the early development period so as to provide the basis for improving the reliability of software. Application to a digital control software system indicates that this method can predict the reliability of software in the early development period, especially in the requirement period and outline design period, effectively
Keywords
aircraft computers; aircraft control; program testing; safety-critical software; software fault tolerance; digital control software system; digital flight control system; early development period; error avoidance measures; error detection; fault tolerance; mission path analysis; mission software; module characteristics; outline design period; software development; software reliability prediction; Application software; Computer errors; Control systems; Digital control; Fault diagnosis; Information analysis; Programming; Software reliability; Software systems; Software testing;
fLanguage
English
Publisher
ieee
Conference_Titel
Digital Avionics Systems Conference, 2000. Proceedings. DASC. The 19th
Conference_Location
Philadelphia, PA
Print_ISBN
0-7803-6395-7
Type
conf
DOI
10.1109/DASC.2000.886881
Filename
886881
Link To Document