查詢結果分析
相關文獻
- Fuzzy Flight Control System for Decoupling Supersonic Missile
- Fuzzy Supervisory Predictive PID Control of a Plastics Extruder Barrel
- 反傳遞模糊類神經網路於流量推估之應用
- Landmark-based Guidance of an Autonomous Vehicle Using Fuzzy Logic Velocity Control and Real-Time Computer Vision
- 模糊理論在時間延遲系統上之研究
- 太陽光電能供電與照明系統(7)--模糊控制之太陽光電能併網供電系統
- 外氣空調之節能恆溫控制
- 規則庫控制法在混合式隔振系統之應用
- Experimental Implementations of Decoupling Self-Organizing Fuzzy Control to a TITO Pneumatic Force Control System
- 模糊船舶航向控制器設計
頁籤選單縮合
題 名 | Fuzzy Flight Control System for Decoupling Supersonic Missile=超音速飛彈之解藕連模糊控制系統設計 |
---|---|
作 者 | 蔡添壽; | 書刊名 | 國立虎尾科技大學學報 |
卷 期 | 26:1 2007.03[民96.03] |
頁 次 | 頁31-41 |
分類號 | 447.5 |
關鍵詞 | 模糊控制; 飛行控制系統; 氣動力解藕; Fuzzy control; Flight control system; Aerodynamic decoupling; |
語 文 | 英文(English) |
中文摘要 | 本文根據傳統飛行控制系統設計技術與經驗,提出模糊解藕連飛行控制系統設計,模糊控制法則的兩個輸入參數為可量測的加速度資料,此模糊控制法則可以簡單的被運用來對付單軸與雙軸大操縱命令飛行操作,得到的結果與傳統的設計相當,但方法較簡單,不需要多維增益值查表,所有的分析結果都經含不確定性與大系統變異之五自由度飛行模擬驗證。 |
英文摘要 | In this literature, a fuzzy control technique is proposed for analyses and designs of a serious aerodynamic coupled skid-to-turn supersonic missile. Fuzzy decoupling logic is developed from conventional design techniques and experiences with two measurable accelerations. It can be easily applied to cope with large single-axis and double-axis maneuvers simultaneously. The fuzzy control system provides simple manner to get same robustness comparing to those of conventional designs technique. All analyzed results are verified by 5-DOF simulations under system variations and uncertainties. |
本系統中英文摘要資訊取自各篇刊載內容。