DO-178C aligned airborne software development, control system design, and simulation — supporting civil and defense aerospace programmes from DAL-E through DAL-A.
The DO-178C certification lifecycle defines the structured framework for demonstrating that airborne software complies with regulatory safety requirements. Objective-based assurance processes cover planning, requirements, design, coding, verification, traceability, structural coverage, and certification evidence — aligned with 14 CFR Part 25 and EASA CS-25. Our engineers have operated within DO-178C processes across real aerospace programmes and understand what Level-A evidence packages look like in practice.
Software lifecycle plans (PSAC, SDP, SVP, SCMP) structured to satisfy FAA and EASA certification expectations at every Design Assurance Level.
Model-based design of flight control, actuation, and avionics algorithms — with simulation and formal verification aligned to DO-178C objectives.
Statement, decision, and MC/DC coverage analysis for DAL-A software — with independent review and objective evidence packages ready for DER review.
A structured technical introduction to the DO-178C airborne software certification lifecycle — covering planning documents, DAL assignments, structural coverage requirements, and certification evidence. Written by engineers with hands-on experience across real aerospace programmes.
Control system design for airborne applications
Control system simulation and virtual validation
Embedded coding aligned to DO-178C objectives
Software lifecycle planning — PSAC, SDP, SVP, SCMP
Structural coverage analysis to MC/DC for DAL-A/B software
Our roadmap includes intelligent traceability and evidence generation tools — automatically linking requirements, design, code, and test results to DO-178C objectives.
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