Software Development and Verification of Critical Flight Control Computer component, which executes the flight law to let aircraft fly in a required direction with a set speed. It also includes the preparation of certification documents in accordance with DO-178C DAL C and ARP4754A.
Technology highlights: C, CAN Aerospace, Arinc429, Matlab/Simulink, RTOS, PowerPC, DO-178C, ARP4754A Size and duration: 3 engineers, 8 months.
Success statement: The prototype was developed, debugged on the test bench and passed to the Customer.
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We consider cooperation with Advalange as one of the strong sides of our project, since we are always sure the solution comes on a high level of quality and we can always rely on timely assistance.
— Christopher Schropp, Head of Technical Development