Robust Stabilization of Oblique Wing Aircraft Model Using PID Controller

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F70883521%3A28140%2F15%3A43873373" target="_blank" >RIV/70883521:28140/15:43873373 - isvavai.cz</a>

Result on the web

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DOI - Digital Object Identifier

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Result language

angličtina

Original language name

Robust Stabilization of Oblique Wing Aircraft Model Using PID Controller

Original language description

The paper is focused on computation of all possible robustly stabilizing Proportional-Integral-Derivative (PID) controllers for oblique wing aircraft modelled as interval system. The main idea of the proposed method is based on Tan's technique for calculation of (nominally) stabilizing PI and PID controllers or robustly stabilizing PI controllers by means of plotting the stability boundary locus in either P-I plane or P-I-D space. Refinement of the existing method by consideration of 16 segment plants instead of 16 Kharitonov plants provides an elegant and efficient tool for finding all robustly stabilizing PID controllers for an interval system.

Czech name

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Czech description

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Type

D - Article in proceedings

CEP classification

BC - Theory and management systems

OECD FORD branch

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Project

Result was created during the realization of more than one project. More information in the Projects tab.

Continuities

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

Publication year

2015

Confidentiality

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

Article name in the collection

IFAC Proceedings Volumes (IFAC-PapersOnline)

ISBN

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ISSN

1474-6670

e-ISSN

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Number of pages

6

Pages from-to

264-269

Publisher name

IFAC Secretariat

Place of publication

Praha

Event location

Bratislava

Event date

Jul 8, 2015

Type of event by nationality

WRD - Celosvětová akce

UT code for WoS article

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