Publication Details
HIL Simulation of a Light Aircraft Flight Control System
HIL, simulation, LSA, light aircraft, aircraft, airplane, SimStar, CANaero, PFD, EMA, autopilot
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.
@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"
}