AIRCRAFT FAULT DIAGNOSIS SYSTEM DEVELOPMENT
Dichotomizing algorithms of diagnostics and reconfiguration of the navigation system which process indicators of inertial, satellite and optical subsystems in real time for typical types of refusals are considered in the work. The given approach provides majority diagnostics of measuring system with...
Main Authors: | Ivan Zhezhera, Ouissam Boudiba |
---|---|
Format: | Article |
Language: | English |
Published: |
Scientific Route OÜ
2017-11-01
|
Series: | Technology Transfer: Fundamental Principles and Innovative Technical Solutions |
Subjects: | |
Online Access: | http://eu-jr.eu/ttfpits/article/view/471 |
Similar Items
-
Implementation of Logic Fault Tolerance on a Dynamically Reconfigurable FPGA
by: Jayarama, Kiran
Published: (2016) -
SRAM based FPGA system capable of runtime fault tolerance and recovery
by: Xu Weijie, et al.
Published: (2019-07-01) -
A COMPETITIVE RECONFIGURATION APPROACH TO AUTONOMOUS FAULT HANDLING USING GENETIC ALGORITHMS
by: Zhang, Kening
Published: (2008) -
Savior: A Reliable Fault Resilient Router Architecture for Network-on-Chip
by: Ayaz Hussain, et al.
Published: (2020-10-01) -
Augmentation of situational awareness by fault passage indicators in distribution network incorporating network reconfiguration
by: Tanmay Jain, et al.
Published: (2019-12-01)