About: Effect of the Pilot Behavior Model on the Helicopter Stability in the Auto-Stabilization System Failure

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About: Effect of the Pilot Behavior Model on the Helicopter Stability in the Auto-Stabilization System Failure Goto Sponge NotDistinct Permalink

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rdf:type	skos:Concept http://linked.opendata.cz/ontology/domain/vavai/Vysledek
rdfs:seeAlso	http://vavtest.unob.cz/registr
Description	This paper describes a mathematical identification of time constants for pilot behavior during a helicopter control process. Based on this mathematical identification and a mathematical description of helicopter dynamics, a simulation scheme was built in the Simulink® environment. Subsequently, the analysis of time constant changes in a pilot behavior model during helicopter longitudinal motion was done, including changes in transfer delay as well as in pilot’s gain. The obtained results are presented in the selected examples in the form of 3D graphs, all created in MATLAB®. This paper describes a mathematical identification of time constants for pilot behavior during a helicopter control process. Based on this mathematical identification and a mathematical description of helicopter dynamics, a simulation scheme was built in the Simulink® environment. Subsequently, the analysis of time constant changes in a pilot behavior model during helicopter longitudinal motion was done, including changes in transfer delay as well as in pilot’s gain. The obtained results are presented in the selected examples in the form of 3D graphs, all created in MATLAB®. (en)
Title	Effect of the Pilot Behavior Model on the Helicopter Stability in the Auto-Stabilization System Failure Effect of the Pilot Behavior Model on the Helicopter Stability in the Auto-Stabilization System Failure (en)
skos:prefLabel	Effect of the Pilot Behavior Model on the Helicopter Stability in the Auto-Stabilization System Failure Effect of the Pilot Behavior Model on the Helicopter Stability in the Auto-Stabilization System Failure (en)
skos:notation	RIV/60162694:G43__/12:00477213!RIV13-MO0-G43_____
http://linked.open...avai/riv/aktivita	I
http://linked.open...avai/riv/aktivity	I
http://linked.open...vai/riv/dodaniDat	2013
http://linked.open...aciTvurceVysledku	Jalovecký, Rudolf Bořil, Jan
http://linked.open.../riv/druhVysledku	D - Článek ve sborníku
http://linked.open...iv/duvernostUdaju	S - Úplné a pravdivé údaje nepodléhající ochraně podle zvláštních právních předpisů
http://linked.open...titaPredkladatele	Ministerstvo obrany / Univerzita obrany - Fakulta vojenských technologií Brno
http://linked.open...dnocenehoVysledku	133323
http://linked.open...ai/riv/idVysledku	RIV/60162694:G43__/12:00477213
http://linked.open...riv/jazykVysledku	eng - angličtina
http://linked.open.../riv/klicovaSlova	MATLAB-Simulink®; Pilot Behavior Model; Helicopter Dynamics; Auto-Stabilization System; Mechatronic Sytem Pilot - Helicopter (en)
http://linked.open.../riv/klicoveSlovo	Auto-Stabilization System Helicopter Dynamics MATLAB-Simulink® Mechatronic Sytem Pilot - Helicopter Pilot Behavior Model
http://linked.open...ontrolniKodProRIV	[ED40E2E90CD3]
http://linked.open...v/mistoKonaniAkce	Rome-Italy
http://linked.open...i/riv/mistoVydani	Italy
http://linked.open...i/riv/nazevZdroje	ESTEL 2012 Proceedings
http://linked.open...in/vavai/riv/obor	JU
http://linked.open...ichTvurcuVysledku	2 (xsd:int)
http://linked.open...cetTvurcuVysledku	2 (xsd:int)
http://linked.open...UplatneniVysledku	2012
http://linked.open...iv/tvurceVysledku	Jalovecký, Rudolf Bořil, Jan
http://linked.open...vavai/riv/typAkce	WRD - Světová
http://linked.open.../riv/zahajeniAkce	2012-01-01 (xsd:date)
number of pages	4 (xsd:int)
http://purl.org/ne...btex#hasPublisher	Neuveden
https://schema.org/isbn	978-1-4673-4688-7
http://localhost/t...ganizacniJednotka	G43
is http://linked.open...avai/riv/vysledek of	Effect of the Pilot Behavior Model on the Helicopter Stability in the Auto-Stabilization System Failure

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