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Detail publikačního výsledku
CHUDÝ, P.; DITTRICH, P.; RZUCIDŁO, P.
Originální název
HIL Simulation of a Light Aircraft Flight Control System
Anglický název
Druh
Stať ve sborníku v databázi WoS či Scopus
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.
Anglický abstrakt
Klíčová slova
HIL, simulation, LSA, light aircraft, aircraft, airplane, SimStar, CANaero, PFD, EMA, autopilot
Klíčová slova v angličtině
Autoři
Rok RIV
2013
Vydáno
17.08.2012
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
URL
http://ieeexplore.ieee.org/xpl/articleDetails.jsp?arnumber=6382395
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" }