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dc.contributor.authorLiang, Yew-Wenen_US
dc.contributor.authorChen, Jun-Yuen_US
dc.contributor.authorJhu, Wei-Mingen_US
dc.date.accessioned2015-07-21T08:31:17Z-
dc.date.available2015-07-21T08:31:17Z-
dc.date.issued2013-01-01en_US
dc.identifier.isbn978-1-4799-2384-7; 978-1-4799-2383-0en_US
dc.identifier.issnen_US
dc.identifier.urihttp://hdl.handle.net/11536/125023-
dc.description.abstractThis paper deals with the design of a robust guidance law for missiles in the presence of unknown target maneuver. Under the design, the closed-loop guidance system is shown to be robust to the target maneuver. Additionally, the scheme presented possesses the flexibility of allowing the engineer to select a desired guidance law for the nominal system (i.e., system without target maneuver) so that the state response of the overall uncertain guidance system is close to that of the selected nominal closed-loop guidance system. The simulation results clearly demonstrate the benefits of the presented scheme.en_US
dc.language.isoen_USen_US
dc.titleA Robust Guidance Law with Predictable Performanceen_US
dc.typeProceedings Paperen_US
dc.identifier.journal2013 CACS INTERNATIONAL AUTOMATIC CONTROL CONFERENCE (CACS)en_US
dc.citation.spage62en_US
dc.citation.epage67en_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:000349259200010en_US
dc.citation.woscount0en_US
Appears in Collections:Conferences Paper