Publication Details

HIL Simulation of a Light Aircraft Flight Control System

CHUDÝ, P.; DITTRICH, P.; RZUCIDŁO, P. HIL Simulation of a Light Aircraft Flight Control System. In Proceedings of the 31st Digital Avionics Systems Conference. Williamsburg, VA: IEEE Computer Society, 2012. p. 1-11. ISBN: 978-1-4673-1699-6.
Czech title
HIL Simulace řídícího systému malého sportovního letounu
Type
conference paper
Language
English
Authors
Chudý Peter, doc. Ing., Ph.D., MBA (DCGM)
Dittrich Petr, Ing., Ph.D.
Rzucidlo Pawel
URL
Keywords

HIL, simulation, LSA, light aircraft, aircraft, airplane, SimStar, CANaero, PFD, EMA, autopilot

Abstract

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.

Published
2012
Pages
1–11
Proceedings
Proceedings of the 31st Digital Avionics Systems Conference
ISBN
978-1-4673-1699-6
Publisher
IEEE Computer Society
Place
Williamsburg, VA
EID Scopus
2-s2.0-84872464778
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"
}
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