DocumentCode :
1496664
Title :
X-33 redundancy management system
Author :
Bolduc, L.P.
Author_Institution :
Aerosp. Electron. Syst., Honeywell Int. Inc., Columbia, MD
Volume :
16
Issue :
5
fYear :
2001
fDate :
5/1/2001 12:00:00 AM
Firstpage :
23
Lastpage :
28
Abstract :
The X-33 is an unmanned advanced technology demonstrator with a mission to validate new technologies for the next generation of Reusable Launch Vehicles. Various system redundancies are designed in the X-33 to enhance the probability of successfully completing its mission in the event of faults and failures during flight. One such redundant system is the Vehicle and Mission Computer that controls the X-33 ea, and manages the avionics subsystems. Historically, redundancy management and applications such as flight control and vehicle management tended to be highly coupled. One of the technologies that the X-33 will demonstrate is the Redundancy Management System (RMS) that uncouples the applications from the redundancy management details, in the same way that real-time operating systems have uncoupled applications from task scheduling, communication and synchronization details
Keywords :
aerospace control; real-time systems; redundancy; space vehicles; X-33 redundancy management system; avionics subsystems; flight control; real-time operating systems; reusable launch vehicles; synchronization details; system redundancies; task scheduling; unmanned advanced technology demonstrator; vehicle management; Aerospace control; Aerospace electronics; Application software; Computer architecture; Fault detection; Hardware; Physics computing; Redundancy; Technology management; Vehicles;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems Magazine, IEEE
Publisher :
ieee
ISSN :
0885-8985
Type :
jour
DOI :
10.1109/62.925693
Filename :
925693
Link To Document :
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