Result Details
HIL Simulation of a Light Aircraft Flight Control System
Dittrich Petr, Ing., Ph.D., DCGM (FIT)
Rzucidlo Pawel
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.
HIL, simulation, LSA, light aircraft, aircraft, airplane, SimStar, CANaero, PFD, EMA, autopilot
@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"
}
Smart Autopilot, TAČR, Program aplikovaného výzkumu a experimentálního vývoje ALFA, TA01010678, start: 2011-01-01, end: 2013-12-31, completed