Design by extrapolation: An evaluation of fault tolerant avionics

IEEE Aerospace and Electronic Systems Magazine

Volumn 17, Issue 4, 2002, Pages 17-25

  Hammett, Robert ^a  

^a CHARLES STARK DRAPER LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AEROSPACE ENGINEERING; CLOSED LOOP CONTROL SYSTEMS; EVALUATION; FAILURE ANALYSIS; FAULT TOLERANT COMPUTER SYSTEMS; SENSORS; SYSTEMS ENGINEERING;

AVIONICS SYSTEMS; FAULT TOLERANT AVIONICS; FAULT TOLERANT SYSTEM;

AVIONICS;

EID: 0036543005     PISSN: 08858985     EISSN: None     Source Type: Journal    
DOI: 10.1109/62.995184     Document Type: Article

References (13)

1. Blindly following the computer
2. Real-time recovery of fault-tolerant processing elements
3. MIL-STD-2165, Military standard testability program for electronic systems and equipments
4. The byzantine generals problem
5. F-16 flight control system redundancy concepts
6. AFTI/F-16 digital flight control computer design
7. Transport engine control design
8. Triple-triple redundant 777 primary flight control computer
9. The airplane information management system, an integrated real-time flight deck control system
10. Next generation fault-tolerant guidance and navigation unit for the inertial upper stage
11. Redundancy management for the X-33 vehicle and mission computer