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"
}