Algebraic ?-Synthesis: Control of the HIMAT Aircraft

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F70883521%3A28140%2F09%3A63507838" target="_blank" >RIV/70883521:28140/09:63507838 - 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

Algebraic ?-Synthesis: Control of the HIMAT Aircraft

Original language description

The algebraic approach is applied to the control of the HIMAT aircraft. The objective is to find a robust controller which guarantees robust stability and decoupled control of longitudinal model of a scaled remotely controlled vehicle version of the advanced fighter HIMAT. Control design is performed by decoupling the MIMO system into two identical SISO plants, which are approximated by a 4th order transfer function. The algebraic approach is then used for pole placement design and the nominal closed-loop poles are tuned so that the peak of the ?-function is minimal. As an optimization tool evolutionary algorithm Differential Migration is used in order to overcome the multimodality of the cost function. Final controllers are compared with the D-K iteration through simulations of standard longitudinal manoeuvres.

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

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Continuities

Z - Vyzkumny zamer (s odkazem do CEZ)

Publication year

2009

Confidentiality

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

Article name in the collection

European Control Conference 2009

ISBN

978-963-311-369-1

ISSN

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e-ISSN

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Number of pages

6

Pages from-to

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Publisher name

EUCA

Place of publication

San Ramon

Event location

Budapest, Hungary

Event date

Aug 26, 2009

Type of event by nationality

WRD - Celosvětová akce

UT code for WoS article

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