A global non-linear control design for a PVTOL vehicle with aerodynamics

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dc.contributor.authorWood, R.
dc.contributor.authorCazzolato, B.
dc.contributor.authorHalim, D.
dc.contributor.conferenceIEEE Conference on Decision and Control (44th : 2005 : Seville, Spain)
dc.contributor.editorCamacho, E.
dc.date.issued2005
dc.description© Copyright 2006 IEEE
dc.description.abstractNon-linear stabilisation and control of a PVTOL vehicle has received much attention in the literature for the low speed case, where aerodynamic effects can be neglected. In this paper, a non-linear control design is presented for a three degree of freedom "Hovering Rocket" with aerodynamic effects included, such that the controller remains functional at high speeds. Control design is based on a non-linear, decoupling change of coordinates presented by many authors in the past. The decoupled system is then controlled using an optimised cascade approach.
dc.description.statementofresponsibilityR. Wood, B. Cazzolato, D. Halim
dc.identifier.citationProceedings of the 44th IEEE Conference on Decision and Control and the European Control Conference CDC-ECC 2005 / E. F. Camacho (ed.): pp.7478-7483
dc.identifier.doi10.1109/CDC.2005.1583368
dc.identifier.isbn0780395689
dc.identifier.issn0743-1546
dc.identifier.orcidCazzolato, B. [0000-0003-2308-799X]
dc.identifier.urihttp://hdl.handle.net/2440/28797
dc.language.isoen
dc.publisherIEEE
dc.publisher.placeCD ROM
dc.relation.ispartofseriesIEEE Conference on Decision and Control
dc.source.urihttp://ieeexplore.ieee.org/stamp/stamp.jsp?tp=&arnumber=1583368
dc.titleA global non-linear control design for a PVTOL vehicle with aerodynamics
dc.typeConference paper
pubs.publication-statusPublished

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