Detail publikace
HIL Simulation of a Light Aircraft Flight Control System
CHUDÝ, P. DITTRICH, P. RZUCIDŁO, P.
Originální název
HIL Simulation of a Light Aircraft Flight Control System
Typ
článek ve sborníku ve WoS nebo Scopus
Jazyk
angličtina
Originální abstrakt
This paper presents the hardware-in-the-loop simulationsof a hybrid flight control system for a light aircraft consisting ofmechanical, electromechanical and digital components. The simulation wasperformed at a light aircraft simulation lab SimStar at Brno University ofTechnology. The aim was the validation and verification of the operationalsuitability of the flight control system's peripherals - electromechanicalactuators, autopilot mode selection panel and a primary flight display. Theinvestigated peripheral devices were connected to SimStar's network using CANaerocommunication protocol. The simulations were focused on the real time automaticflight control modes operational scenarios.
Klíčová slova
HIL, simulation, LSA, light aircraft, aircraft, airplane, SimStar, CANaero, PFD, EMA, autopilot
Autoři
CHUDÝ, P.; DITTRICH, P.; RZUCIDŁO, P.
Rok RIV
2012
Vydáno
17. 8. 2012
Nakladatel
IEEE Computer Society
Místo
Williamsburg, VA
ISBN
978-1-4673-1699-6
Kniha
Proceedings of the 31st Digital Avionics Systems Conference
Strany od
1
Strany do
11
Strany počet
11
URL
BibTex
@inproceedings{BUT97022,
author="Peter {Chudý} and Petr {Dittrich} and Pawel {Rzucidlo}",
title="HIL Simulation of a Light Aircraft Flight Control System",
booktitle="Proceedings of the 31st Digital Avionics Systems Conference",
year="2012",
pages="1--11",
publisher="IEEE Computer Society",
address="Williamsburg, VA",
isbn="978-1-4673-1699-6",
url="http://ieeexplore.ieee.org/xpl/articleDetails.jsp?arnumber=6382395"
}