Title :
Advanced avionics system architecture
Author :
Fabian, Gordon R. ; Rayl, Timothy R.
Author_Institution :
Adv. Syst., Rockwell Collins, Cedar Rapids, IA, USA
fDate :
31 Oct-7 Nov 1998
Abstract :
The Collins Advanced Avionics System Architecture uses an increased amount of integration to provide an unprecedented level of functional capability, fault tolerance and flexibility, as well as on-board diagnostic aids and other features designed to reduce crew work load and enhance the availability of system functions. Large format liquid crystal flight displays (LCD) and cursor control devices with voice activation integrate the display and control of system functions. This lessens crew work load while reducing the number of system displays and controls, providing a more intuitive cockpit. Functional processing is accomplished in an integrated processing center (IPC) using standardized modules and virtual machine/partitioned processing and field-loadable software. This provides a flexible, cost effective, reusable architecture with inherent growth capability and true software mobility. The digital communication network achieves total connectivity among all subsystems. The connectivity is accomplished with data concentrators for legacy equipment and high speed digital local area network hubs for internal IPC data, IPC to IPC communication, and interface to other high data rate users. This significantly reduces system latencies, cross cockpit wiring and individual I/O connections
Keywords :
aircraft computers; aircraft displays; digital communication; embedded systems; fault tolerant computing; local area networks; advanced avionics system architecture; cost effective reusable architecture; crew work load; cursor control devices; data concentrators; digital communication network; embedded processor; fault tolerance; field-loadable software; flexibility; functional capability; functional processing; high speed digital LAN hubs; inherent growth capability; integrated processing center; large format liquid crystal flight displays; legacy equipment; life cycle cost; more intuitive cockpit; on-board diagnostic aids; standardized modules; total connectivity among subsystems; true software mobility; virtual machine/partitioned processing; voice activation; Aerospace electronics; Communication system control; Computer architecture; Control systems; Costs; Fault tolerant systems; Liquid crystal devices; Liquid crystal displays; Software reusability; Virtual machining;
Conference_Titel :
Digital Avionics Systems Conference, 1998. Proceedings., 17th DASC. The AIAA/IEEE/SAE
Conference_Location :
Bellevue, WA
Print_ISBN :
0-7803-5086-3
DOI :
10.1109/DASC.1998.739843