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Development of Verification Environment for Flight Safety Critical Software using NEXUS

NEXUS를 이용한 비행안전 필수 소프트웨어 검증환경 개발

  • Received : 2012.02.19
  • Accepted : 2012.06.01
  • Published : 2012.06.01

Abstract

Verification and validation of operational software of the flight control computer, which is flight safety critical, is very important to prove correctness and faultness of the software. To verify the real-time softare requirement on operational software of flight control computer, real-time software internal parameter and variable monitoring technics on hardware-in-the-loop environment, similar to on-flight environment, is required. This paper describes flight safety critical software validation and verificiation environment using standard debugging interface, NEXUS 5001.

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Cited by

  1. A Software-Based Monitoring Framework for Time-Space Partitioned Avionics Systems vol.5, 2017, https://doi.org/10.1109/ACCESS.2017.2755638
  2. A Study on Software Based Fault-Tolerance Techniques for Flight Control Computer vol.44, pp.3, 2016, https://doi.org/10.5139/JKSAS.2016.44.3.256