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 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.

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

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"
}