完整後設資料紀錄
DC 欄位語言
dc.contributor.authorWang, Chi-Hsuen_US
dc.contributor.authorChen, Chun-Yaoen_US
dc.date.accessioned2014-12-08T15:36:45Z-
dc.date.available2014-12-08T15:36:45Z-
dc.date.issued2014en_US
dc.identifier.isbn978-1-4799-3106-4en_US
dc.identifier.issn1810-7869en_US
dc.identifier.urihttp://hdl.handle.net/11536/25126-
dc.description.abstractIn this paper, an adaptive recurrent neural network (RNN) controller is proposed for missile guidance. We address the problem of one agent (defending missiles) and one target (incoming missiles) in air battle scenario. The RNN controller is designed to force an agent (or defending missile) toward a target (or incoming missile), and a monitoring controller is also designed to reduce the error between the RNN controller and ideal one. The former is the main controller that can be easily designed. Its weighting factors are activated to dispatch the agent toward the target. By using the Lyapunov constraints, we update the weighting factors for the proposed RNN controller to guarantee the stability of the path evolution (or planning) system. Excellent simulation results are obtained by using this new approach for missile guidance, which show that our RNN has the lowest average miss distance (MD) among the several techniques.en_US
dc.language.isoen_USen_US
dc.subjectMissile guidanceen_US
dc.subjectrecurrent neural network (RNN)en_US
dc.subjectLyapunov constraintsen_US
dc.titleIntelligent Missile Guidance by Using Adaptive Recurrent Neural Networksen_US
dc.typeProceedings Paperen_US
dc.identifier.journal2014 IEEE 11TH INTERNATIONAL CONFERENCE ON NETWORKING, SENSING AND CONTROL (ICNSC)en_US
dc.citation.spage559en_US
dc.citation.epage564en_US
dc.contributor.department交大名義發表zh_TW
dc.contributor.department電機工程學系zh_TW
dc.contributor.departmentNational Chiao Tung Universityen_US
dc.contributor.departmentDepartment of Electrical and Computer Engineeringen_US
dc.identifier.wosnumberWOS:000341938800097-
顯示於類別:會議論文