Requirements for future advanced tactical aircraft identify the need for flight control system architectures that provide a higher degree of performance with regard to electromagnetic interference immunity, communication bus data rate, propulsion/utility subsystem integration, and affordability. Evolution for highly centralized, digital, fly-by-light flight/propulsion/utility control system is achieved as modular functions are implemented and integrated by serial digital fiberoptic communication links. These adaptable architectures allow the user to configure the fly- by-light system to meet unique safety requirements, system performance, and design-to-cost targets. This paper presents results of the open and closed loop system demonstrations of Fly-By-Light Advanced System Hardware architecture building blocks integrated with SAE AS-1773 communication bus at MDA.
Demonstration results of fly-by-light flight control system architectures for tactical military aircraft
Fly-by-Light III ; 1996 ; Denver,CO,United States
Proc. SPIE ; 2840
1996-10-14
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
CNS/ATM for Tactical Military Aircraft
British Library Conference Proceedings | 2003
|CNS/ATM for tactical military aircraft
IEEE | 2003
|