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Statements

Subject Item
n2:RIV%2F00216305%3A26230%2F12%3APU101847%21RIV13-MSM-26230___
rdf:type
skos:Concept n21:Vysledek
rdfs:seeAlso
http://ieeexplore.ieee.org/xpl/articleDetails.jsp?arnumber=6382395
dcterms:description
This paper presents the hardware-in-the-loop simulations of a hybrid flight control system for a light aircraft consisting of mechanical, electromechanical and digital components. The simulation was performed at a light aircraft simulation lab SimStar at Brno University of Technology. The aim was the validation and verification of the operational suitability of the flight control system's peripherals - electromechanical actuators, autopilot mode selection panel and a primary flight display. The investigated peripheral devices were connected to SimStar's network using CANaero communication protocol. The simulations were focused on the real time automatic flight control modes operational scenarios. This paper presents the hardware-in-the-loop simulations of a hybrid flight control system for a light aircraft consisting of mechanical, electromechanical and digital components. The simulation was performed at a light aircraft simulation lab SimStar at Brno University of Technology. The aim was the validation and verification of the operational suitability of the flight control system's peripherals - electromechanical actuators, autopilot mode selection panel and a primary flight display. The investigated peripheral devices were connected to SimStar's network using CANaero communication protocol. The simulations were focused on the real time automatic flight control modes operational scenarios.
dcterms:title
HIL Simulation of a Light Aircraft Flight Control System HIL Simulation of a Light Aircraft Flight Control System
skos:prefLabel
HIL Simulation of a Light Aircraft Flight Control System HIL Simulation of a Light Aircraft Flight Control System
skos:notation
RIV/00216305:26230/12:PU101847!RIV13-MSM-26230___
n21:predkladatel
n23:orjk%3A26230
n3:aktivita
n4:P n4:Z
n3:aktivity
P(TA01010678), Z(MSM0021630528)
n3:dodaniDat
n15:2013
n3:domaciTvurceVysledku
Chudý, Peter n17:1744887
n3:druhVysledku
n10:D
n3:duvernostUdaju
n19:S
n3:entitaPredkladatele
n20:predkladatel
n3:idSjednocenehoVysledku
139048
n3:idVysledku
RIV/00216305:26230/12:PU101847
n3:jazykVysledku
n7:eng
n3:klicovaSlova
HIL, simulation, LSA, light aircraft, aircraft, airplane, SimStar, CANaero, PFD, EMA, autopilot
n3:klicoveSlovo
n5:light%20aircraft n5:aircraft n5:CANaero n5:simulation n5:airplane n5:EMA n5:HIL n5:SimStar n5:PFD n5:autopilot n5:LSA
n3:kontrolniKodProRIV
[13922C2A2D5F]
n3:mistoKonaniAkce
Williamsburg, VA
n3:mistoVydani
Williamsburg, VA
n3:nazevZdroje
Proceedings of the 31st Digital Avionics Systems Conference
n3:obor
n24:IN
n3:pocetDomacichTvurcuVysledku
2
n3:pocetTvurcuVysledku
3
n3:projekt
n12:TA01010678
n3:rokUplatneniVysledku
n15:2012
n3:tvurceVysledku
Rzucidlo, Pawel Chudý, Peter Dittrich, Petr
n3:typAkce
n9:WRD
n3:zahajeniAkce
2012-10-14+02:00
n3:zamer
n6:MSM0021630528
s:numberOfPages
11
n22:hasPublisher
IEEE Computer Society
n13:isbn
978-1-4673-1699-6
n16:organizacniJednotka
26230