
G05D1/0077- Control of position, course or altitude of land, water, air, or space vehicles, e.g. G05D1/0055- Control of position, course or altitude of land, water, air, or space vehicles, e.g. G05D1/00- Control of position, course or altitude of land, water, air, or space vehicles, e.g. G05D- SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.) Filing date Publication date Priority claimed from US76424568A external-priority Application filed by Bendix Corp filed Critical Bendix Corp Publication of GB1249700A publication Critical patent/GB1249700A/en Status Expired legal-status Critical Current Links Original Assignee Bendix Corp Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.) Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.) Expired Application number GB46811/69A Current Assignee (The listed assignees may be inaccurate. Google Patents Triple redundant flight control system Google Patents GB1249700A - Triple redundant flight control system Through substantial and sustained internal R&D, as well as through participation in international R&D-programs, we ensure that our offering stays world class.GB1249700A - Triple redundant flight control system We can deliver complete systems from the cockpit lever to the flap/slat surface. We offer electromechanically based High Lift systems of both centrally driven and distributed architectures, and work with both slats (leading edge) and flaps (trailing edge) systems. Saab is an experienced supplier of High Lift systems and is present on both military and commercial aircraft. Our computer offering is based on a common module product platform allowing for cost-efficient customization. Saab offers primary flight control systems, among things, specifically tailored for a helicopter’s challenging environmental requirements and high demands for weight-efficiency. We have experience from both fixed wing and rotary wing UAVs.
Saab offers complete size and weight efficient primary flight control systems, ranging from safety critical real time flight control computers through sensors and control electronics to electromechanical actuators. The system is scalable and have the capability to also serve the secondary features on the aircraft.
Saab's primary actuator system is developed as a modular system with adaptation of a wide range of existing components. Primary Flight Electromechanical Actuation 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). Key ElementsĮxample of Flight Control Systems program: Primary Flight Control for fixed wing aircraft All products are based on a modularized product platform allowing cost-efficient customization of each configuration. Besides primary Flight Control, our target applications within secondary flight controls are slat (leading edge), flap (trailing edge), trim and spoiler/airbrake systems. Our offering includes both integrated and distributed systems.
Redundant flight control system software#
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.
With our capabilities we can provide the complete system from cockpit controls through safety-critical control computers and motor control electronics to electromechanical actuators.