Polynomial LPV synthesis applied to turbofan engines

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21230%2F10%3A00161838" target="_blank" >RIV/68407700:21230/10:00161838 - 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
Polynomial LPV synthesis applied to turbofan engines
Original language description
Results on polynomial fixed-order controller design are extended to SISO gain-scheduling with guaranteed stability and H1 performance over the whole scheduling parameter range. Salient features of the approach are:(a)the use of polynomials as modeling objects;(b)the use of flexible linear matrix inequalities (LMI) conditions allowing polynomial dependence of the open-loop system and controller transfer functions in the scheduling parameters;and(c) the decouplingin the LMI conditions between the Lyapunovvariables and the controller variables,allowing both parameter-dependent Lyapunov functions and fixed-order controller design.The synthesis procedure is integrated into the ATOL framework developed by the manufacturer of aircraft and space engines Snecma to systematically design reduced complexity gain-scheduled control laws for aircraft turbofan engines.
Czech name
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Czech description
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Type
J<sub>x</sub> - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)
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
Z - Vyzkumny zamer (s odkazem do CEZ)

Publication year
2010
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

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