Full metadata record
DC Field | Value | Language |
---|---|---|
dc.contributor.author | 毛修羽 | en_US |
dc.contributor.author | Mao, Xiu-Yu | en_US |
dc.contributor.author | 高一智 | en_US |
dc.contributor.author | Gao, Yi-Zhi | en_US |
dc.date.accessioned | 2014-12-12T02:02:35Z | - |
dc.date.available | 2014-12-12T02:02:35Z | - |
dc.date.issued | 1982 | en_US |
dc.identifier.uri | http://140.113.39.130/cdrfb3/record/nctu/#NT714146010 | en_US |
dc.identifier.uri | http://hdl.handle.net/11536/51685 | - |
dc.description.abstract | 當一高性能飛彈運作於其任務中時,由於飛行高度和速度的隨時不同,飛彈氣動力轉 換函數將發生快速而巨大的改變本文將探討如何設計一自適性自動駛儀,俾能克服上 述狀況的影響,而能有近似的響應。 文中就兩類設計方式,分基於明顯式的和隱含式的參數判別方法,提出三計。此三種 設計均以數位系模擬研究其結果,並比較和評估此三者之適用性。 | zh_TW |
dc.language.iso | zh_TW | en_US |
dc.subject | 自適性 | zh_TW |
dc.subject | 自動駕駛儀 | zh_TW |
dc.subject | 氣動力轉換函數 | zh_TW |
dc.subject | 明顯式參數判別法 | zh_TW |
dc.subject | 隱含式參數判別法 | zh_TW |
dc.subject | 數位系統 | zh_TW |
dc.subject | 自動控制 | zh_TW |
dc.subject | 控制工程 | zh_TW |
dc.subject | 電腦 | zh_TW |
dc.subject | AUTOMATIC-CONTROL-ENGINEERING | en_US |
dc.subject | CONTROL-ENGINEERING | en_US |
dc.subject | COMPUTER | en_US |
dc.title | 自適性自動駕駛儀設計 | zh_TW |
dc.type | Thesis | en_US |
dc.contributor.department | 電控工程研究所 | zh_TW |
Appears in Collections: | Thesis |