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CHUDÝ, P.; DITTRICH, P.; RZUCIDŁO, P.
Original Title
HIL Simulation of a Light Aircraft Flight Control System
English Title
Type
Paper in proceedings (conference paper)
Original 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.
English abstract
Keywords
HIL, simulation, LSA, light aircraft, aircraft, airplane, SimStar, CANaero, PFD, EMA, autopilot
Key words in English
Authors
RIV year
2013
Released
17.08.2012
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
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" }