Powerplant Control System Tuning Activities

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dc.contributor.authorEsen, C.
dc.contributor.authorYalcinkaya, H.M.
dc.contributor.authorZengin, E.
dc.contributor.authorSansal, K.
dc.contributor.authorEzertas, A.A.
dc.contributor.authorTarhan, H.E.
dc.date.accessioned2026-08-11T11:54:40Z
dc.date.issued2023
dc.description.abstractT-625 helicopter is a light utility multi role helicopter that is designed by Turkish Aerospace Helicopter Group. It is equipped with twin CTS800-4AT turboshaft engines developed by the Light Helicopter Turbine Engine Company (LHTEC). Engines are controlled by an advanced, redundant dual-channel full authority digital engine control (FADEC) system. This paper presents aspects of the load anticipation and dynamic response characterization of engine control system in powerplant integration process of T-625 helicopter, together with the results of engine control tuning flight test campaign which are performed to fine-tune FADEC controller parameters during flight.
dc.identifier.urihttps://hdl.handle.net/20.500.11881/4547
dc.language.isoen
dc.subject.otherTest & Evaluation
dc.titlePowerplant Control System Tuning Activities

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