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Global stabilization of axial compressors using nonlinear cancellation and backstepping designs

dc.citation.epage1361en_US
dc.citation.issue12en_US
dc.citation.spage1345en_US
dc.citation.volume29en_US
dc.citation.woscount2
dc.contributor.authorLiaw, DCen_US
dc.contributor.authorHuang, JTen_US
dc.contributor.department電控工程研究所zh_TW
dc.contributor.departmentInstitute of Electrical and Control Engineeringen_US
dc.date.accessioned2014-12-08T15:47:22Z
dc.date.available2014-12-08T15:47:22Z
dc.date.issued1998-12-01en_US
dc.description.abstractIssues concerning the global stabilization of axial compressors are presented Instead of locally stabilizing the bifurcated rotating stall equilibria to avoid suddern performance drop, control schemes are proposed to globally stabilize the unstalled nominal operating paints. These are achieved by employing nonlinear cancellation and backstepping designs via either throttle or direct mass flow rate control if the compressor characteristic satisfies the 'left-tilt' property. The designs not only guarantee a safe operation close to the maximum achievable pressure rise, but the bifurcated system equilibria are also found to be stabilized due to the elimination of the jump phenomenon. Though both throttle and direct mass flow rate control schemes can be implemented for global stabilization, numerical simulations demonstrate that direct mass flow rate control achieves better post-stall system behaviour.en_US
dc.identifier.issn0020-7721en_US
dc.identifier.journalINTERNATIONAL JOURNAL OF SYSTEMS SCIENCEen_US
dc.identifier.urihttps://ir.lib.nycu.edu.tw/handle/11536/31749
dc.identifier.wosnumberWOS:000077594800001
dc.language.isoen_USen_US
dc.titleGlobal stabilization of axial compressors using nonlinear cancellation and backstepping designsen_US
dc.typeArticleen_US

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