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 (FIT)
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 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.

Published
2012
Pages
1–11
Proceedings
Proceedings of the 31st Digital Avionics Systems Conference
Conference
31st Digital Avionics Systems Conference, Williamsburg, VA, US
ISBN
978-1-4673-1699-6
Publisher
IEEE Computer Society
Place
Williamsburg, VA
EID Scopus
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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