HW in-the-Loop Simulation of a Light Aircraft Autopilot

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26230%2F13%3APU106420" target="_blank" >RIV/00216305:26230/13:PU106420 - isvavai.cz</a>

Výsledek na webu

<a href="http://arc.aiaa.org/doi/abs/10.2514/6.2013-4829?prevSearch=&searchHistoryKey=" target="_blank" >http://arc.aiaa.org/doi/abs/10.2514/6.2013-4829?prevSearch=&searchHistoryKey=</a>

DOI - Digital Object Identifier

<a href="http://dx.doi.org/10.2514/6.2013-4829" target="_blank" >10.2514/6.2013-4829</a>

Jazyk výsledku

angličtina

Název v původním jazyce

HW in-the-Loop Simulation of a Light Aircraft Autopilot

Popis výsledku v původním jazyce

Hardware in the loop simulations are undisputably perceived as an integral part of the avionics design and development process. This paper describes the simulation process which has been employed to test a digital autopilot for a light sport aircraft. Simulation processes have been performed on two different ground testing levels. The first setting consisted of a laboratory grade verification phase which supported the initial functional estimate of the designed and implemented autopilot features. The subsequent testing level already included the embedded autopilot system installation on board of the test aircraft. The initial hardware in the loop simulation was performed at the light aircraft simulation lab SimStar at the Brno University of Technology. The aim of the ground simulations was to verify and ground test the operational suitability of the designed autopilot flight control system elements. The implemented flight control system hardware units have been connected into the simulation network using the CANaerospace communication protocol for both testing scenarios. Simulations focused on the real time automatic flight modes operational scenarios. Both of the simulation scenarios confirmed the anticipated performance of the autopilot design features.

Název v anglickém jazyce

HW in-the-Loop Simulation of a Light Aircraft Autopilot

Popis výsledku anglicky

Hardware in the loop simulations are undisputably perceived as an integral part of the avionics design and development process. This paper describes the simulation process which has been employed to test a digital autopilot for a light sport aircraft. Simulation processes have been performed on two different ground testing levels. The first setting consisted of a laboratory grade verification phase which supported the initial functional estimate of the designed and implemented autopilot features. The subsequent testing level already included the embedded autopilot system installation on board of the test aircraft. The initial hardware in the loop simulation was performed at the light aircraft simulation lab SimStar at the Brno University of Technology. The aim of the ground simulations was to verify and ground test the operational suitability of the designed autopilot flight control system elements. The implemented flight control system hardware units have been connected into the simulation network using the CANaerospace communication protocol for both testing scenarios. Simulations focused on the real time automatic flight modes operational scenarios. Both of the simulation scenarios confirmed the anticipated performance of the autopilot design features.

Druh

D - Stať ve sborníku

CEP obor

—

OECD FORD obor

20206 - Computer hardware and architecture

Projekt

Výsledek vznikl pri realizaci vícero projektů. Více informací v záložce Projekty.

Návaznosti

P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Rok uplatnění

2013

Kód důvěrnosti údajů

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Název statě ve sborníku

Conference Proceeding Series (GNC/AFM/MST)

ISBN

978-1-62993-153-1

ISSN

—

e-ISSN

—

Počet stran výsledku

11

Strana od-do

1-11

Název nakladatele

American Institute of Aeronautics and Astronautics

Místo vydání

Boston, MA

Místo konání akce

Boston, Massachusetts

Datum konání akce

19. 8. 2013

Typ akce podle státní příslušnosti

WRD - Celosvětová akce

Kód UT WoS článku

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