Fault Tolerant EHA Architectures

IEEE Aerospace and Electronic Systems Magazine

Volumn 7, Issue 3, 1992, Pages 32-42

  Sadeghi, Tom ^a   Lyons, Arthur ^b  

^a BINGHAMTON UNIVERSITY   (United States)

^b GENERAL ELECTRIC COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT, MILITARY; COMPUTER SYSTEMS, DIGITAL - FAULT TOLERANT CAPABILITY; PROBABILITY; REDUNDANCY; RELIABILITY - ANALYSIS;

ELECTROHYDROSTATIC ACTUATOR; MISSION SUCCESS PROBABILITY; PROBABILITY OF LOSS OF CONTROL; PROBABILITY OF MISSION ABORT;

ACTUATORS;

EID: 0026840181     PISSN: 08858985     EISSN: None     Source Type: Journal    
DOI: 10.1109/62.141899     Document Type: Article

References (9)

1. A. Escobosa (10/90) All Digital Electro Hydrostatic Servoactuator Interactive Control Technologies, Inc. Paper No. 901900, Aerospace Technology Conference
2. R. Crocco (5/90) Electro Hydrostatic Systems General Electric-Aircraft Control Systems Department SAE-7E Aerospace Electronics and Equipment Conference
3. R. VanNocker (5/90) EH A Loading on a 270 Vdc Bus General Electric-Aircraft Control Systems Department SAE-7C Systems Conference
4. H. Geminder (5/90) Electro Hydrostatic Actuation Systems Allied Signal Aerospace Company SAE-7 Conference
5. W. Hartnett EH A Stiffness General Electric-Aircraft Control Systems Department SAE-6D Conference
6. R. Crocco NAECON 90 Electro Hydrostatic Actuation System Trade Offs, General Electric-Aircraft Control Systems Department NAECON 90
7. F. El-Sherif (5/90) X-MA Flight Control System Actuator Allied Signal Aerospace Company SAE-A6
8. T. Sadeghi, P. Shannon, F. Motamed Fault Tolerant Flight Critical System Architecture Comparisons GE-ACSD NAECON 91
9. Osder, S. Chronological Overview of Past Avionic Flight Control System Realibilitv in Military and Commercial Applications, N77-25057, AIAA.