Synthesis of invariant circuit angular stabilization of unmanned aircraft at the pitch angle

The article considers the synthesis methods of an automatic invariant system of the pitch angle stabilization of an unmanned aerial vehicle that is based on the concept of inverse dynamics problems. The methods and results of simulation mathematical results of synthesized stabilization loop with usi...

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Main Author: I. V. Rozhkov
Format: Article
Language:English
Published: Belarusian National Technical University 2020-09-01
Series:Системный анализ и прикладная информатика
Subjects:
Online Access:https://sapi.bntu.by/jour/article/view/479
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author I. V. Rozhkov
author_facet I. V. Rozhkov
author_sort I. V. Rozhkov
collection DOAJ
description The article considers the synthesis methods of an automatic invariant system of the pitch angle stabilization of an unmanned aerial vehicle that is based on the concept of inverse dynamics problems. The methods and results of simulation mathematical results of synthesized stabilization loop with using the Simulink of program MATLAB. The results of a comparative analysis of the dynamic characteristics of the contour of angular stabilization of an unmanned aerial vehicle by pitch angle with a PID-controller and a synthesized robust controller are presented.
format Article
id doaj-art-aa5554cfbdb14ceb94c33f92ef58851b
institution Kabale University
issn 2309-4923
2414-0481
language English
publishDate 2020-09-01
publisher Belarusian National Technical University
record_format Article
series Системный анализ и прикладная информатика
spelling doaj-art-aa5554cfbdb14ceb94c33f92ef58851b2025-02-03T11:37:39ZengBelarusian National Technical UniversityСистемный анализ и прикладная информатика2309-49232414-04812020-09-0103142010.21122/2309-4923-2020-3-14-20362Synthesis of invariant circuit angular stabilization of unmanned aircraft at the pitch angleI. V. Rozhkov0Belarusian State Academy of AviationThe article considers the synthesis methods of an automatic invariant system of the pitch angle stabilization of an unmanned aerial vehicle that is based on the concept of inverse dynamics problems. The methods and results of simulation mathematical results of synthesized stabilization loop with using the Simulink of program MATLAB. The results of a comparative analysis of the dynamic characteristics of the contour of angular stabilization of an unmanned aerial vehicle by pitch angle with a PID-controller and a synthesized robust controller are presented.https://sapi.bntu.by/jour/article/view/479unmanned aerial vehiclerobust automatic stabilization systeminverse dynamics problemsmathematical model of an unmanned aerial vehicle
spellingShingle I. V. Rozhkov
Synthesis of invariant circuit angular stabilization of unmanned aircraft at the pitch angle
Системный анализ и прикладная информатика
unmanned aerial vehicle
robust automatic stabilization system
inverse dynamics problems
mathematical model of an unmanned aerial vehicle
title Synthesis of invariant circuit angular stabilization of unmanned aircraft at the pitch angle
title_full Synthesis of invariant circuit angular stabilization of unmanned aircraft at the pitch angle
title_fullStr Synthesis of invariant circuit angular stabilization of unmanned aircraft at the pitch angle
title_full_unstemmed Synthesis of invariant circuit angular stabilization of unmanned aircraft at the pitch angle
title_short Synthesis of invariant circuit angular stabilization of unmanned aircraft at the pitch angle
title_sort synthesis of invariant circuit angular stabilization of unmanned aircraft at the pitch angle
topic unmanned aerial vehicle
robust automatic stabilization system
inverse dynamics problems
mathematical model of an unmanned aerial vehicle
url https://sapi.bntu.by/jour/article/view/479
work_keys_str_mv AT ivrozhkov synthesisofinvariantcircuitangularstabilizationofunmannedaircraftatthepitchangle