Detail publikace

HIL Simulation of a Light Aircraft Flight Control System

Originální název

HIL Simulation of a Light Aircraft Flight Control System

Anglický název

HIL Simulation of a Light Aircraft Flight Control System

Jazyk

en

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.

Anglický 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.

BibTex


@inproceedings{BUT97022,
  author="Peter {Chudý} and Petr {Dittrich} and Pawel {Rzucidlo}",
  title="HIL Simulation of a Light Aircraft Flight Control System",
  annote="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.",
  address="IEEE Computer Society",
  booktitle="Proceedings of the 31st Digital Avionics Systems Conference",
  chapter="97022",
  edition="NEUVEDEN",
  howpublished="electronic, physical medium",
  institution="IEEE Computer Society",
  year="2012",
  month="august",
  pages="1--11",
  publisher="IEEE Computer Society",
  type="conference paper"
}