The use of the localization method for calculation of the robust PID regulator parameters for unmanned aircraft servo motor

The problem of controlling a typical nonlinear servo motor of an unmanned aercraft with non-stationary parameters using a robust PID controller is considered. The procedure for calculating the parameters of a robust PID controller based on the localization method (further - LM PID controller) for co...

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Main Authors: A. A. Sanko, A. A. Sheinikov, T. A. Tishchenko, D. A. Smolskiy
Format: Article
Language:Russian
Published: Moscow State Technical University of Civil Aviation 2020-02-01
Series:Naučnyj Vestnik MGTU GA
Subjects:
Online Access:https://avia.mstuca.ru/jour/article/view/1639
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spelling doaj-9af0cd349e3147c88a68a10063106fc72021-07-28T21:00:43ZrusMoscow State Technical University of Civil Aviation Naučnyj Vestnik MGTU GA2079-06192542-01192020-02-012319510510.26467/2079-0619-2020-23-1-95-1051342The use of the localization method for calculation of the robust PID regulator parameters for unmanned aircraft servo motorA. A. Sanko0A. A. Sheinikov1T. A. Tishchenko2D. A. Smolskiy3Belarusian State Academy of AviationMilitary Academy of the Republic of BelarusBelarusian State Academy of AviationBelarusian State Academy of AviationThe problem of controlling a typical nonlinear servo motor of an unmanned aercraft with non-stationary parameters using a robust PID controller is considered. The procedure for calculating the parameters of a robust PID controller based on the localization method (further - LM PID controller) for continuous and discrete control systems is studied. The influence of disturbing factors (internal and external) acting on the servo motor is considered. It is established that the main perturbations acting on the servo drive include internal perturbations, which are changes in the time constant and its gain from the temperature of the environment and the quality of the supply voltage. The simulation in the class of linear and nonlinear continuous systems showed that a servo drive with a ML PID controller has the property of robustness in the working range of changes in both the input signal and the parameters of the servo drive and controller. Simulation results showing the research are presented. When describing a servo motor with an LM PID controller in the class of linear discrete systems, its robustness is limited by a narrow range of variation of both its parameters and the quantization period of the input signal. As the degree of uncertainty in the parameters of the servo motor increases (approaching the working range of their change), the discrete system loses stability. For the synthesis of robust control circuits of an unmanned aercraft with given characteristics, mathematical dependences of the settling time and static error of a typical servo motor with LM PID controller from the quantization period of the input signal and the degree of uncertainty in its parameters are presented.https://avia.mstuca.ru/jour/article/view/1639control systemservomotorsrobust pid controllertransition processeslocalization method
collection DOAJ
language Russian
format Article
sources DOAJ
author A. A. Sanko
A. A. Sheinikov
T. A. Tishchenko
D. A. Smolskiy
spellingShingle A. A. Sanko
A. A. Sheinikov
T. A. Tishchenko
D. A. Smolskiy
The use of the localization method for calculation of the robust PID regulator parameters for unmanned aircraft servo motor
Naučnyj Vestnik MGTU GA
control system
servomotors
robust pid controller
transition processes
localization method
author_facet A. A. Sanko
A. A. Sheinikov
T. A. Tishchenko
D. A. Smolskiy
author_sort A. A. Sanko
title The use of the localization method for calculation of the robust PID regulator parameters for unmanned aircraft servo motor
title_short The use of the localization method for calculation of the robust PID regulator parameters for unmanned aircraft servo motor
title_full The use of the localization method for calculation of the robust PID regulator parameters for unmanned aircraft servo motor
title_fullStr The use of the localization method for calculation of the robust PID regulator parameters for unmanned aircraft servo motor
title_full_unstemmed The use of the localization method for calculation of the robust PID regulator parameters for unmanned aircraft servo motor
title_sort use of the localization method for calculation of the robust pid regulator parameters for unmanned aircraft servo motor
publisher Moscow State Technical University of Civil Aviation
series Naučnyj Vestnik MGTU GA
issn 2079-0619
2542-0119
publishDate 2020-02-01
description The problem of controlling a typical nonlinear servo motor of an unmanned aercraft with non-stationary parameters using a robust PID controller is considered. The procedure for calculating the parameters of a robust PID controller based on the localization method (further - LM PID controller) for continuous and discrete control systems is studied. The influence of disturbing factors (internal and external) acting on the servo motor is considered. It is established that the main perturbations acting on the servo drive include internal perturbations, which are changes in the time constant and its gain from the temperature of the environment and the quality of the supply voltage. The simulation in the class of linear and nonlinear continuous systems showed that a servo drive with a ML PID controller has the property of robustness in the working range of changes in both the input signal and the parameters of the servo drive and controller. Simulation results showing the research are presented. When describing a servo motor with an LM PID controller in the class of linear discrete systems, its robustness is limited by a narrow range of variation of both its parameters and the quantization period of the input signal. As the degree of uncertainty in the parameters of the servo motor increases (approaching the working range of their change), the discrete system loses stability. For the synthesis of robust control circuits of an unmanned aercraft with given characteristics, mathematical dependences of the settling time and static error of a typical servo motor with LM PID controller from the quantization period of the input signal and the degree of uncertainty in its parameters are presented.
topic control system
servomotors
robust pid controller
transition processes
localization method
url https://avia.mstuca.ru/jour/article/view/1639
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