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Algebraic μ-synthesis: Control of the HIMAT aircraft

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dc.title Algebraic μ-synthesis: Control of the HIMAT aircraft en
dc.contributor.author Dlapa, Marek
dc.relation.ispartof 2009 European Control Conference, ECC 2009
dc.identifier.isbn 978-395241739-3
dc.date.issued 2009
dc.citation.spage 573
dc.citation.epage 578
dc.event.title 2009 10th European Control Conference, ECC 2009
dc.event.location Budapest
utb.event.state-en Hungary
utb.event.state-cs Maďarsko
dc.event.sdate 2009-08-23
dc.event.edate 2009-08-26
dc.type conferenceObject
dc.language.iso en
dc.publisher Institute of Electrical and Electronics Engineers (IEEE)
dc.relation.uri http://ieeexplore.ieee.org/xpls/abs_all.jsp?arnumber=7074464
dc.description.abstract 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 μ-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. © 2009 EUCA. en
utb.faculty Faculty of Applied Informatics
dc.identifier.uri http://hdl.handle.net/10563/1004558
utb.identifier.obdid 43859046
utb.identifier.scopus 2-s2.0-84955176631
utb.source d-scopus
dc.date.accessioned 2015-05-28T11:39:21Z
dc.date.available 2015-05-28T11:39:21Z
utb.contributor.internalauthor Dlapa, Marek
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