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2002, vol. 1, iss. 2, pp. 40-45
Turbojet engine diagnostic system
Military Technical Institute - MTI, Belgrade
Keywords: fly-by-wire control system; digital electronic control; turbojet engine; airforce equipment; diagnostic system
Abstract
This paper presents a concept of digital electronic control of turbojet engines as a basis for engine diagnostic system operation in real time. It was started from baseline system, which provides a minimum of required reliability without redundancy. In order to increase a reliability of baseline control system, it is shown a way for selective redundancy.
References
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article language: Serbian
document type: Original Scientific Paper
published in SCIndeks: 21/07/2007

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