Menu
Home
Contact us
Stats
Categories
Calendar
Toggle Wiki
Wiki Home
Last Changes
Rankings
List pages
Orphan pages
Sandbox
Print
Toggle Image Galleries
Galleries
Rankings
Toggle Articles
Articles home
List articles
Rankings
Toggle Blogs
List blogs
Rankings
Toggle Forums
List forums
Rankings
Toggle File Galleries
List galleries
Rankings
Toggle Maps
Mapfiles
Toggle Surveys
List surveys
Stats
ITHEA Classification Structure > B. Hardware  > B.8 PERFORMANCE AND RELIABILITY > B.8.1 Reliability, Testing, and Fault-Tolerance
THE INFORMATION-ANALYTICAL SYSTEM FOR DIAGNOSTICS ...
By: Ilya Prokoshev, Vyacheslav Suminov (2925 reads)
Rating: (1.00/10)

Abstract: The operation of technical processes requires increasingly advanced supervision and fault diagnostics to improve reliability and safety. This paper gives an introduction to the field of fault detection and diagnostics and has short methods classification. Growth of complexity and functional importance of inertial navigation systems leads to high losses at the equipment refusals. The paper is devoted to the INS diagnostics system development, allowing identifying the cause of malfunction. The practical realization of this system concerns a software package, performing a set of multidimensional information analysis. The project consists of three parts: subsystem for analyzing, subsystem for data collection and universal interface for open architecture realization. For a diagnostics improving in small analyzing samples new approaches based on pattern recognition algorithms voting and taking into account correlations between target and input parameters will be applied. The system now is at the development stage.

Keywords: technical diagnostics, fault detection, inertial navigation system, navigation, aircraft units, supervision, monitoring, fault diagnostics, diagnostic reasoning

ACM Classification Keywords: B.8.1 Reliability, Testing, and Fault-Tolerance?; J.2 Computer Applications: Physical Sciences and Engineering: Aerospace

Link:

THE INFORMATION-ANALYTICAL SYSTEM FOR DIAGNOSTICS OF AIRCRAFT NAVIGATION UNITS

Ilya Prokoshev, Vyacheslav Suminov

http://www.foibg.com/ijita/vol13/ijita13-2-p04.pdf

Print
B.8.1 Reliability, Testing, and Fault-Tolerance
article: TWO-LEVEL GENETIC ALGORITHM FOR PROGRAMMABLE LOGIC DEVICES RECONFIGURATION · RESEARCH OF ACCURACY OF GUARANTEED OPERAYTING TIME PREDICTION BY FRACTILE ... · IMAGE SENSORS IN SECURITY AND MEDICAL APPLICATIONS ... · THE INFORMATION-ANALYTICAL SYSTEM FOR DIAGNOSTICS ... · PARAMETRIC IDENTIFICATION AND DIAGNOSIS OF INTEGRATED ... ·
Login
[ register | I forgot my password ]
World Clock
Powered by Tikiwiki Powered by PHP Powered by Smarty Powered by ADOdb Made with CSS Powered by RDF powered by The PHP Layers Menu System
RSS Wiki RSS Blogs rss Articles RSS Image Galleries RSS File Galleries RSS Forums RSS Maps rss Calendars
[ Execution time: 0.08 secs ]   [ Memory usage: 7.51MB ]   [ GZIP Disabled ]   [ Server load: 0.44 ]
Powered by Tikiwiki CMS/Groupware