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dc.contributor.author陳昌宏en_US
dc.contributor.authorChen, Chung-Hungen_US
dc.contributor.author陳永平en_US
dc.contributor.authorChen Yon-Pingen_US
dc.date.accessioned2014-12-12T02:15:01Z-
dc.date.available2014-12-12T02:15:01Z-
dc.date.issued1995en_US
dc.identifier.urihttp://140.113.39.130/cdrfb3/record/nctu/#NT840327053en_US
dc.identifier.urihttp://hdl.handle.net/11536/60311-
dc.description.abstract本論文的主題為順滑模態的飛行控制器設計。將整個系統分成縱向運 動和橫向運動並加以線性化之後設計控制器。其中,由於引擎十分複雜而 難以用數學模型加以描述,因此將速度分開以PI控制器設計。在飛行的路 徑規劃上是希望飛機能夠完成一爬升轉彎和水平加速的動作,並將模態追 隨的技術運用在控制命令的產生上,以期能將飛行的姿態順滑化。所採用 的模擬環境為在1991年AIAA會議中所提出的飛行模擬系統。 This thesis is on sliding mode flight control 。The system is divided into two parts ( longitudinal and lateral)。 Linearization is employed prior to controller design。Due to the engine complexity,velocity control is accomplished by using a PI compensator 。In flight schedule,the climb-turn and level accelerations of the aircraft are achieved via sliding mode。 Moreover,we use the model following technique to generate commands that smooth the flight path。zh_TW
dc.language.isozh_TWen_US
dc.subject順滑模態zh_TW
dc.subject飛行控制zh_TW
dc.subject模態追隨zh_TW
dc.subject比例積分控制zh_TW
dc.subjectsliding modeen_US
dc.subjectflight controlen_US
dc.subjectmodel followingen_US
dc.subjectPI controlen_US
dc.title模態追隨技術運用在順滑模態飛行控制器設計zh_TW
dc.titlemodel-following technique applied to sliding mode flight cotroller designen_US
dc.typeThesisen_US
dc.contributor.department電控工程研究所zh_TW
Appears in Collections:Thesis