Eaton required avionics software design, integration and verification for an over-wing Air-to-Air Refuelling Pod control system, with full compliance to system requirements and programme milestones.
KDC Projects operated as a fixed-price, task-driven delivery partner, undertaking requirements capture, architecture definition, software development, integration, test and debugging across control and fault display modules.
This established compliant, verified software baselines, reduced integration risk, and supported assured progression toward system qualification and programme delivery.
Requirement
Capture and analyse system requirements, design the solution architecture, develop and integrate the avionics software, and perform comprehensive testing, debugging, and verification to ensure full compliance of an over wing Air-to-Air Refuelling Pod control system.
Skills & Tools
- Enterprise Architect
- All Change
- Helix QAC
- Windriver Debugger
Tasking
Production of the Software Design Specification. Integration, Test and debugging of the Software code for the modules that control the switching between the Over Wing pods and the Fault Display.
Deliverables
- Production of the Control & Fault Display Design Specification
- Integration and Test of the above Software Code
- Debugging Support and issue resolution as required
Outcome
KDC Projects continue to support Eaton with SQEP personnel to deliver specialist tasking over an 18-month program which is on schedule to complete in 2026.