LQR Based Digital Autopilot For Light Sport Aircraft

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26230%2F22%3APU147438" target="_blank" >RIV/00216305:26230/22:PU147438 - isvavai.cz</a>

Výsledek na webu

<a href="https://www.icas.org/ICAS_ARCHIVE/ICAS2022/data/papers/ICAS2022_0719_paper.pdf" target="_blank" >https://www.icas.org/ICAS_ARCHIVE/ICAS2022/data/papers/ICAS2022_0719_paper.pdf</a>

DOI - Digital Object Identifier

—

Jazyk výsledku

angličtina

Název v původním jazyce

LQR Based Digital Autopilot For Light Sport Aircraft

Popis výsledku v původním jazyce

This paper addresses research on modern methods in automatic Flight Control System design and evaluation, as seen from the perspective of state-of-the-art and future utilization on Unmanned Aerial Systems. The paper introduces a Flight Control System design process with a special emphasis on the Model-Based Design approach. An integral part of this process is the composition of the aircrafts mathematical model employed in the flight control laws synthesis and the development of a simulation framework for the evaluation of the automatic Flight Control System's stability and performance.The core of this work is aimed at flight control laws synthesis built around the optimal control theory. The researched flight control laws originating from the proposed design process were integrated into an experimental digital Flight Control System.

Název v anglickém jazyce

LQR Based Digital Autopilot For Light Sport Aircraft

Popis výsledku anglicky

This paper addresses research on modern methods in automatic Flight Control System design and evaluation, as seen from the perspective of state-of-the-art and future utilization on Unmanned Aerial Systems. The paper introduces a Flight Control System design process with a special emphasis on the Model-Based Design approach. An integral part of this process is the composition of the aircrafts mathematical model employed in the flight control laws synthesis and the development of a simulation framework for the evaluation of the automatic Flight Control System's stability and performance.The core of this work is aimed at flight control laws synthesis built around the optimal control theory. The researched flight control laws originating from the proposed design process were integrated into an experimental digital Flight Control System.

Druh

D - Stať ve sborníku

CEP obor

—

OECD FORD obor

20206 - Computer hardware and architecture

Projekt

<a href="/cs/project/8A19003" target="_blank" >8A19003: Framework of key enabling technologies for safe and autonomous drones' applications</a><br>

Návaznosti

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

Rok uplatnění

2022

Kód důvěrnosti údajů

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

Název statě ve sborníku

33rd Congress of the International Council of the Aeronautical Sciences, ICAS 2022

ISBN

978-1-7138-7116-3

ISSN

2958-4647

e-ISSN

—

Počet stran výsledku

15

Strana od-do

5321-5335

Název nakladatele

International Council of the Aeronautical Sciences

Místo vydání

Stockholm

Místo konání akce

Stockholm

Datum konání akce

4. 9. 2022

Typ akce podle státní příslušnosti

EUR - Evropská akce

Kód UT WoS článku

—