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article: 1 from 1  
2005, vol. 4, iss. 3-4, pp. 49-53
Architecture of microprocessor control systems in aviation engines
Military Technical Institute - MTI, Belgrade
Keywords: aviation engine; electronic control system; architecture of microprocessor control systems
Abstract
This paper deals with two redundant control system architectures applied on modern fighter aircraft. A non redundant engine control system whose desired reliability can be established using different levels of the redundancy of subsystems components, is presented, too.
References
Landy, J.R., Yonke, A.W., Stewart, F.J. (1987) Development of HIDEC adaptive engine control systems. Transactions of the ASME, vol. 109, str. 146-151
Timothy, J.L. (1987) Microprocessor-based engine control. in: 23th Joint Propulsion Conference 87, AIAA June 29-July 2, San Diego, California
Vujić, D. (1998) Osnovni koncept sistema elektronskog upravljanja turbomlaznim motorima. Naučno-tehnički pregled, vol. 48, br. 5, str. 39-44
Vujić, D. (1997) Prilog elektronskom upravljanju turbomlaznim motorima. in: Vazduhoplovstvo '97, Međunarodni naučno-stručni skup, Beograd, 11-12 decembar, zbornik radova, str. C43-C48
Vujić, D. (1998) Uticaj konfiguracije elektronskih sistema upravljanja na pouzdanost i održavanje turbomlaznih motora. in: SYM-OP-IS '98, (XXV) Jubilarni jugoslovenski simpozijum o operacionim istraživanjima, Herceg Novi, 21-24. sep., zbornik radova, str. 531-534
Warner, D.E., Hermann, H.W. (1982) Reliability design study for a fault-tolerant electronic engine control. in: AIAA/SAE/ASME 18th Joint Propulsion Conference, Cleveland, Ohio, June 21-23
 

About

article language: Serbian
document type: Professional Paper
published in SCIndeks: 02/06/2007

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