Electronic flight instrument system

for aircraft

With our capabilities we can provide the complete system from cockpit controls through safety-critical control computers and motor control electronics to electromechanical actuators. We can also supply software to the customer desired level, from Board Support Package (BSP) through Boot Code, Device Drivers, Built-In-Test, Operating Systems to Application Software. Our offering includes both integrated and distributed systems. Besides primary Flight Control, our target applications within secondary flight controls are slat (leading edge), flap (trailing edge), trim and spoiler/airbrake systems. All products are based on a modularized product platform allowing cost-efficient customization of each configuration. Key Elements Rapid prototyping, short lead time to first equipment with full functional compliance RTCA DO-178/254 DAL A compliant RTCA DO-160 compliant (environmental) EASA and FAA certified products Model-based software development Safety critical control computers yet with high level of integrated platform functionality, examples: ARINC standard dataloader AFDX Extensive Built-In Tests (PBIT, CBIT and IBIT) RTOS (ARINC653) Primary Flight Control for fixed wing aircraft Saab has proven expertise in developing real time safety-critical control computers for fixed wing flight control and provides in-house development of both HW and SW (including application SW). Our computer offering is based on a common module product platform allowing for cost-efficient customization.