The gas turbine aero-engine control systems over the past eight decades have been thoroughly investigated. This review purposes are to present a comprehensive reference for aero-engine control desi...

https://journals.sagepub.com/doi/pdf/10.1177/0020294020956675

A scientometric analysis and critical review of gas turbine aero-engines control: From Whittle engine to more-electric propulsion

The basic operating principles of an electronic digital computer gas turbine engine control system are presented. Closed loop turbine discharge temperature and speed controls have been implemented; their feasibility was demonstrated through hybrid digital/analog simulation and actual tests of a GE J85 turbojet engine through the start mode to maximum afterburner. Control mode description and results of the analysis and experimental runs are given in this paper.Copyright © 1968 by ASME

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R. M. Frazzini

Papers

DIGATEC (Digital Gas Turbine Engine Control)