AvionicsOps: Kontinuierliches Avionik-DevSecOps & DO-178C Werkzeugqualifikation

AvionicsOps verbindet moderne CI/CD-Pipelines mit strengen Lufttüchtigkeitsstandards und automatisiert MC/DC-Testabdeckung, statische Code-Analyse und DO-330-Qualifikation für DO-178C DAL A Flugsoftware.

AvionicsOps Automated Continuous Certification & CI/CD Pipeline

Git commit trigger, static analysis gate, MC/DC target test runner, and automated PSAC generator

Central System: Airborne DevSecOps Orchestrator - DO-178C / DO-330 Verification Engine

Aviation Architecture Nodes

  • Safety-Critical Git Repository
  • Static Code & MISRA-C Linter
  • Target Hardware-in-the-Loop Runner
  • Automated MC/DC Coverage Analyzer
  • Airworthiness Evidence Vault

Architectural Layers & Protocol Stacks

  • Deterministic Code Governance & Standards (GitLab CI / Gitea / Signed Commits / MISRA-C:2012): Enforcing strict coding standards, banning dynamic memory allocation, and verifying cryptographic commit signatures.
  • Automated Static & Structural Analysis (Astrée / Polyspace / SonarQube Aerospace Edition): Mathematically proving the absence of runtime errors: buffer overflows, division by zero, and dead code.
  • Hardware-in-the-Loop Automated Execution (Target Emulator & Hardware Test Benches): Compiling with certified compilers (CompCert/Green Hills) and executing test suites directly on flight processors.
  • DO-330 Qualified Evidence Generation (Tool Qualification Kits (TQL-1 to TQL-5)): Generating automated traceability matrices, Plan for Software Aspects of Certification (PSAC), and Software Accomplishment Summaries.

Flight Telemetry Metrics: 100% (MC/DC Branch Coverage for DAL A) | Zero Defect (MISRA-C:2012 Rule Compliance) | DO-330 TQL-1 (Tool Qualification Level) | < 45 min (Full Airborne CI/CD Regression Run)

Avionik-DevSecOps, DO-178C-Tool-Qualifizierung (DO-330) und kontinuierliche Integration von Bordsoftware

Autoritative technische Referenz fuer avionics devsecops, do-178c tool qualification (do-330) & continuous airborne software integration gemaess FAA Part 135, DO-178C DAL A Avionik-Software und ASTM F3411 UTM-Interoperabilitaet.

Core Engineering Areas

Technical Publications

Related Cluster Architecture Specifications