FlightGear Application for Flight Simulation of a mini-UAV

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F70883521%3A28140%2F15%3A43871400" target="_blank" >RIV/70883521:28140/15:43871400 - isvavai.cz</a>

Výsledek na webu

<a href="http://scitation.aip.org/content/aip/proceeding/aipcp/10.1063/1.4912769" target="_blank" >http://scitation.aip.org/content/aip/proceeding/aipcp/10.1063/1.4912769</a>

DOI - Digital Object Identifier

<a href="http://dx.doi.org/10.1063/1.4912769" target="_blank" >10.1063/1.4912769</a>

Jazyk výsledku

angličtina

Název v původním jazyce

FlightGear Application for Flight Simulation of a mini-UAV

Popis výsledku v původním jazyce

This paper presents using of FlightGear application for flight simulation of a mini-UAV (Unmanned Aerial Vehicle). The first part of the paper is about general information of UAVs and about the fundamentals of airplane flight mechanics. The main sectionsummarizes the information about FlightGear application and describes a way of using the application to simulate a mini-UAV. The process of altitude change by using autopilot has been simulated. In the created simulation, three stage cascade controller was used for an altitude control. Heading was controlled by 2 stage cascade PID (Proportional-Integral-Derivative) controller. An automatic throttle system was applied for a velocity control. The setting of all controllers is included in the description of the simulation. Finally, the results of FlightGear simulation are discussed.

Název v anglickém jazyce

FlightGear Application for Flight Simulation of a mini-UAV

Popis výsledku anglicky

This paper presents using of FlightGear application for flight simulation of a mini-UAV (Unmanned Aerial Vehicle). The first part of the paper is about general information of UAVs and about the fundamentals of airplane flight mechanics. The main sectionsummarizes the information about FlightGear application and describes a way of using the application to simulate a mini-UAV. The process of altitude change by using autopilot has been simulated. In the created simulation, three stage cascade controller was used for an altitude control. Heading was controlled by 2 stage cascade PID (Proportional-Integral-Derivative) controller. An automatic throttle system was applied for a velocity control. The setting of all controllers is included in the description of the simulation. Finally, the results of FlightGear simulation are discussed.

Druh

D - Stať ve sborníku

CEP obor

IN - Informatika

OECD FORD obor

—

Projekt

—

Návaznosti

S - Specificky vyzkum na vysokych skolach

Rok uplatnění

2015

Kód důvěrnosti údajů

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

Název statě ve sborníku

AIP Conference Proceedings

ISBN

978-0-7354-1287-3

ISSN

0094-243X

e-ISSN

—

Počet stran výsledku

4

Strana od-do

"nestrankovano"

Název nakladatele

AIP Publishing

Místo vydání

Melville

Místo konání akce

Rhodos

Datum konání akce

22. 9. 2014

Typ akce podle státní příslušnosti

WRD - Celosvětová akce

Kód UT WoS článku

000355339703045