Algebraic μ-synthesis: Control of the HIMAT aircraft

Dlapa, Marek

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.identifier.doi	10.23919/ECC.2009.7074464
dc.relation.uri	https://ieeexplore.ieee.org/document/7074464
dc.relation.uri	https://ieeexplore.ieee.org/stamp/stamp.jsp?tp=&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