Publication detail

HIL Simulation of a Light Aircraft Flight Control System

CHUDÝ, P. DITTRICH, P. RZUCIDŁO, P.

Original Title

HIL Simulation of a Light Aircraft Flight Control System

Type

conference paper

Language

English

Original 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.

Keywords

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

Authors

CHUDÝ, P.; DITTRICH, P.; RZUCIDŁO, P.

RIV year

2012

Released

17. 8. 2012

Publisher

IEEE Computer Society

Location

Williamsburg, VA

ISBN

978-1-4673-1699-6

Book

Proceedings of the 31st Digital Avionics Systems Conference

Pages from

1

Pages to

11

Pages count

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"
}