UNSTABLE STATES STABILIZATION OF THE REVERSE PENDULUM WITH SCREW ACTUATORS

The subject of study in the article is the forming models' process for the angular motion of the rocker with screw electric actuators. The purpose is to develop the approach to the simplest models formation for the angular motion of the rocker with screw electric actuators as the automatic cont...

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Main Authors: Анатолий Степанович Кулик, Евгений Валерьевич Филиппович, Константин Юрьевич Дергачев, Сергей Николаевич Пасичник, Юрий Александрович Немшилов
Format: Article
Language:English
Published: National Aerospace University «Kharkiv Aviation Institute» 2020-06-01
Series:Авіаційно-космічна техніка та технологія
Subjects:
Online Access:http://nti.khai.edu/ojs/index.php/aktt/article/view/1127
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author Анатолий Степанович Кулик
Евгений Валерьевич Филиппович
Константин Юрьевич Дергачев
Сергей Николаевич Пасичник
Юрий Александрович Немшилов
author_facet Анатолий Степанович Кулик
Евгений Валерьевич Филиппович
Константин Юрьевич Дергачев
Сергей Николаевич Пасичник
Юрий Александрович Немшилов
author_sort Анатолий Степанович Кулик
collection DOAJ
description The subject of study in the article is the forming models' process for the angular motion of the rocker with screw electric actuators. The purpose is to develop the approach to the simplest models formation for the angular motion of the rocker with screw electric actuators as the automatic control object. Tasks: to form the physical model of rocker with screw electric actuators. Using the Lagrangian formalism develop the non-linear mathematical description of the angular motion process of a rocker with screw electric actuators. To obtain the linearized mathematical description of the automatic control object in form of state space in the cases when one sensor (angular position) and two sensors (angular position and angular velocity of the rocker) are used. To obtain the description of the automatic control object in the frequency domain using Laplace transforms. To form graphic models of the automatic control object using structural diagrams in the time and frequency domains. To analyze the functional properties of the automatic control object: stability, controllability, observability, structural and signal diagnosability in the cases when one sensor (angular position) and two sensors (angular position and angular velocity of the rocker) are used. To formulate the conditions for using mathematical descriptions as mathematical models of the automatic control object. The methods used are the Lagrange method, analytical linearization, state space, Laplace transform, Lypunov, Kalman criteria, diagnosability. The following results were obtained: the approach to the formation of the simplest models for the angular motion of a rocker with screw electric actuators as an object of automatic control for solving specific problems of analysis and synthesis was formed. Conclusions. The scientific novelty lies in the formation of the approach to the formation of the simplest control models for the angular motion of the rocker with screw electric actuators which differs from the known completeness of accounting for the acting forces and moments.
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spelling doaj.art-2552beabe37244459fbe798dc90e5baa2023-09-02T19:26:54ZengNational Aerospace University «Kharkiv Aviation Institute»Авіаційно-космічна техніка та технологія1727-73372663-22172020-06-010341410.32620/aktt.2020.3.011146UNSTABLE STATES STABILIZATION OF THE REVERSE PENDULUM WITH SCREW ACTUATORSАнатолий Степанович Кулик0Евгений Валерьевич Филиппович1Константин Юрьевич Дергачев2Сергей Николаевич Пасичник3Юрий Александрович Немшилов4Национальный аэрокосмический университет им. Н. Е. Жуковского «Харьковский авиационный институт», ХарьковНациональный аэрокосмический университет им. Н. Е. Жуковского «Харьковский авиационный институт», ХарьковНациональный аэрокосмический университет им. Н. Е. Жуковского «Харьковский авиационный институт», ХарьковНациональный аэрокосмический университет им. Н. Е. Жуковского «Харьковский авиационный институт», ХарьковНациональный аэрокосмический университет им. Н. Е. Жуковского «Харьковский авиационный институт», ХарьковThe subject of study in the article is the forming models' process for the angular motion of the rocker with screw electric actuators. The purpose is to develop the approach to the simplest models formation for the angular motion of the rocker with screw electric actuators as the automatic control object. Tasks: to form the physical model of rocker with screw electric actuators. Using the Lagrangian formalism develop the non-linear mathematical description of the angular motion process of a rocker with screw electric actuators. To obtain the linearized mathematical description of the automatic control object in form of state space in the cases when one sensor (angular position) and two sensors (angular position and angular velocity of the rocker) are used. To obtain the description of the automatic control object in the frequency domain using Laplace transforms. To form graphic models of the automatic control object using structural diagrams in the time and frequency domains. To analyze the functional properties of the automatic control object: stability, controllability, observability, structural and signal diagnosability in the cases when one sensor (angular position) and two sensors (angular position and angular velocity of the rocker) are used. To formulate the conditions for using mathematical descriptions as mathematical models of the automatic control object. The methods used are the Lagrange method, analytical linearization, state space, Laplace transform, Lypunov, Kalman criteria, diagnosability. The following results were obtained: the approach to the formation of the simplest models for the angular motion of a rocker with screw electric actuators as an object of automatic control for solving specific problems of analysis and synthesis was formed. Conclusions. The scientific novelty lies in the formation of the approach to the formation of the simplest control models for the angular motion of the rocker with screw electric actuators which differs from the known completeness of accounting for the acting forces and moments.http://nti.khai.edu/ojs/index.php/aktt/article/view/1127коромысловинтовой электроприводобъект автоматического управленияуправляемостьнаблюдаемостьдиагностируемостьматематические моделипространство состояний
spellingShingle Анатолий Степанович Кулик
Евгений Валерьевич Филиппович
Константин Юрьевич Дергачев
Сергей Николаевич Пасичник
Юрий Александрович Немшилов
UNSTABLE STATES STABILIZATION OF THE REVERSE PENDULUM WITH SCREW ACTUATORS
Авіаційно-космічна техніка та технологія
коромысло
винтовой электропривод
объект автоматического управления
управляемость
наблюдаемость
диагностируемость
математические модели
пространство состояний
title UNSTABLE STATES STABILIZATION OF THE REVERSE PENDULUM WITH SCREW ACTUATORS
title_full UNSTABLE STATES STABILIZATION OF THE REVERSE PENDULUM WITH SCREW ACTUATORS
title_fullStr UNSTABLE STATES STABILIZATION OF THE REVERSE PENDULUM WITH SCREW ACTUATORS
title_full_unstemmed UNSTABLE STATES STABILIZATION OF THE REVERSE PENDULUM WITH SCREW ACTUATORS
title_short UNSTABLE STATES STABILIZATION OF THE REVERSE PENDULUM WITH SCREW ACTUATORS
title_sort unstable states stabilization of the reverse pendulum with screw actuators
topic коромысло
винтовой электропривод
объект автоматического управления
управляемость
наблюдаемость
диагностируемость
математические модели
пространство состояний
url http://nti.khai.edu/ojs/index.php/aktt/article/view/1127
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