HIL Simulation of a Light Aircraft Flight Control System

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26230%2F12%3APU101847" target="_blank" >RIV/00216305:26230/12:PU101847 - isvavai.cz</a>
Result on the web
<a href="http://ieeexplore.ieee.org/xpl/articleDetails.jsp?arnumber=6382395" target="_blank" >http://ieeexplore.ieee.org/xpl/articleDetails.jsp?arnumber=6382395</a>
DOI - Digital Object Identifier
—

Result language
angličtina
Original language name
HIL Simulation of a Light Aircraft Flight Control System
Original language description
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 atBrno 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.
Czech name
—
Czech description
—

Project
<a href="/en/project/TA01010678" target="_blank" >TA01010678: Smart Autopilot</a><br>
Continuities
Z - Vyzkumny zamer (s odkazem do CEZ)

Publication year
2012
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
Proceedings of the 31st Digital Avionics Systems Conference
ISBN
978-1-4673-1699-6
ISSN
—
e-ISSN
—
Number of pages
11
Pages from-to
1-11
Publisher name
IEEE Computer Society
Place of publication
Williamsburg, VA
Event location
Williamsburg, VA
Event date
Oct 14, 2012
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
—

Similar results(10)