Online detection and avoidance of helicopter TGT limits

Ilkay Yavrucuk, Gonenc Gursoy, Yaroslav Novikov

Research output: Contribution to journalConference articlepeer-review

3 Scopus citations

Abstract

Turboshaft engines of rotary-wing aircraft impose limitations on the flight envelope via Turbine Gas Temperature (TGT). Pilots are required to react on possible violations by monitoring TGT limits. For a fly-by-wire system, avoidance of the TGT limit could be accomplished using tactile cues and advanced envelope protection algorithms. In this paper, a neural-network-based adaptive limit detection algorithm is used to estimate approaching TGT violations and the corresponding control limits on the collective control. Collective limits are then used for avoidance of the TGT limit. High fidelity helicopter and engine models are used to show that TGT violations can be estimated with sufficient lead time to warn the pilot using tactile cues.

Original languageEnglish
Pages (from-to)1650-1655
Number of pages6
JournalAnnual Forum Proceedings - AHS International
Volume3
StatePublished - 2013
Externally publishedYes
Event69th American Helicopter Society International Annual Forum 2013 -
Duration: 21 May 201323 May 2013

Fingerprint

Dive into the research topics of 'Online detection and avoidance of helicopter TGT limits'. Together they form a unique fingerprint.

Cite this