A new approach to the mechanization of the traditional navigation function can provide the key integration interface between the flight critical aircraft Fly-By-Wire stabilization and control and the remainder of the mission avionics. Redundant, integrated navigation and sensor assemblies provide all of the aircraft position, velocity, acceleration, angular rate, attitude, heading and air data states needed for both the flight control as well as the mission management functions. The architectural concept uses functional partitioning with distributed processing aimed at decoupling software dependencies between the various integrated avionics system elements.
Helicopter avionics architecture for integrating flight critical functions
Architektur von Helikopteravionik fuer die Integration flugkritischer Funktionen
1986
8 Seiten, 8 Bilder, 1 Tabelle, 15 Quellen
Conference paper
English
Emerald Group Publishing | 1987
|Online Contents | 2002