Avionics

You can benefit from our experience of over 15 years in the development of avionic systems ranging from DAL A to D, such as:

• Navigation systems
• Fuel management systems
• Engine control units
• Blade control
• First level maintenance equipment
• Air data computer
• Cabin equipment

• Conception and execution of safety-related development projects
• Short-term and rapid production of demonstrators and pre-prototypes
• Production of planning documents, such as PHAC/PSAC, SVP/HVP, SCP/HCP
• Production of hardware/software development documents
• System conception and test conception
• Development according to our own or customised design and coding guidelines
• DO-178B/C compliant software
• DO-254 compliant hardware
• DO-254 compliant FPGA firmware
• Verification
• Code review incl. static code analysis
• Unit tests
• Integration tests
• Acceptance test procedures
• Tool qualification (RTCA DO-330)
• Reviews
• Support for and execution of environmental tests to DO-160
• Assistance in the transition to series production
• Support for qualification tests
• Support during the product life cycle
• Obsolescence impact analysis

We work to the following standards and directives among others

• RTCA DO-178B/C and DO-254
• RTCA DO-160
• ARP 4754/4761
• MIL-HDBK 271 and SN 29500
• NATO Quality Assurance Requirements for Software Development (AQAP 150 Machinery Directive: 2006/42/EC)