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dc.contributor.authorLin, CCen_US
dc.contributor.authorChen, FCen_US
dc.date.accessioned2014-12-08T15:40:22Z-
dc.date.available2014-12-08T15:40:22Z-
dc.date.issued2003-09-01en_US
dc.identifier.issn0731-5090en_US
dc.identifier.urihttp://hdl.handle.net/11536/27563-
dc.description.abstractA way to integrate the cerebellar model articulation controller (CMAC) neural network with the missile longitudinal conventional feedback controller (CFC) to compensate for nonlinearities, unmodeled dynamics, parameter variations, etc., is proposed. The inner loop of the CFC will essentially be left unchanged to improve the stability of the missile. The outer loop of CFC, in addition to playing its traditional role, would work with the CMAC to learn quickly to approximate the dynamic inversion from angle of attack to control deflection, to achieve better tracking in normal acceleration. In this arrangement, the well-known CFC acts as a safety net, whereas additional performance is brought about through CMAC learning.en_US
dc.language.isoen_USen_US
dc.titleImproving conventional longitudinal missile autopilot using cerebellar model articulation controller neural networksen_US
dc.typeArticleen_US
dc.identifier.journalJOURNAL OF GUIDANCE CONTROL AND DYNAMICSen_US
dc.citation.volume26en_US
dc.citation.issue5en_US
dc.citation.spage711en_US
dc.citation.epage718en_US
dc.contributor.department電控工程研究所zh_TW
dc.contributor.departmentInstitute of Electrical and Control Engineeringen_US
dc.identifier.wosnumberWOS:000185305200005-
dc.citation.woscount4-
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