自動著陸系統 的英文怎麼說
中文拼音 [zìdòngzhāoliùxìtǒng]
自動著陸系統
英文
autoland system- 自 : Ⅰ代詞(自己) self; oneself; one s own Ⅱ副詞(自然;當然) certainly; of course; naturally; willin...
- 著 : 著助詞1. (表示動作的持續) 2. (表示狀態的持續) 3. (用在動詞或表示程度的形容詞後面, 加強命令或囑咐的語氣) 4. (加在某些動詞後面, 使變成介詞)
- 陸 : 陸數詞(六的大寫) six (used for the numeral 六 on cheques, etc. to avoid mistakes or alterations)
- 系 : 系動詞(打結; 扣) tie; fasten; do up; button up
- 統 : Ⅰ名詞1 (事物間連續的關系) interconnected system 2 (衣服等的筒狀部分) any tube shaped part of ...
- 自動 : 1 (自己主動) voluntarily; of one s own accord 2 (不憑借人為的力量) automatic; spontaneous 3 ...
- 著陸 : landing; land; touch down
- 系統 : 1. (按一定關系組成的同類事物) system 2. (有條理的;有系統的) systematic
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Ailas automatic instrument landing approach system
自動儀表著陸進場系統This algorithm can apply to any real complicated atc enviroment with flexible goal cost function, and static or dynamic real - time atc automation system, to minimize traffic delay and improve landing capacity
該演算法能滿足現實復雜空管條件下的各種限制約束,以及多種目標成本函數,可應用於靜態和動態的實時atc自動化系統,能有效地減小交通延誤和提高著陸容量。This thesis combines artificial neural networks ( nn ) with adaptive inverse control ( nnai ) on the basis of analyzing their principle and characteristics, and applies them in the control of nonlinear system. an application in the design of automatic landing is shown
本文在深入分析了神經網路和自適應逆方法的原理與特點的基礎上,將神經網路與自適應逆方法相結合,著重研究了將這種方法應用於非線性系統的控制問題,最後,用飛機自動著陸的過程,驗證了神經網路自適應逆方法的效果。The flight control system contains gps & ins, which insured auto takeoff & landing, as well as the whole flight process
飛行控制系統採用gps全球定位系統和慣性導航系統,可自動完成從起飛到著陸的整個飛行過程。Applying the direct feedback linearization ( dfl ) method to design the aircraft automatic landing control system model that is overall non - linearization
摘要應用直接反饋線性化的方法來設計非線性飛機模型自動著陸全面控制系統。Firstly, the method of feedback linearization is adopted to design the automatic landing system
論文將非線性系統反饋精確線性化方法應用在飛機自動著陸系統的設計上。Aerospace automatic landing
航空航天自動著陸系統Als aircraft automatilanding system
飛機自動著陸系統Automatic landing system of airplane using adaptive inverse control. traffic accidents occur during landing frequently
自適應逆控制方法在飛機自動著陸系統中的應用。The simulation results show that the designed landing system possesses not only satisfactory performances but also strong robustness
模擬結果說明用非線性控制方法設計的自動著陸系統有較好的魯棒性。The control system for longitudinal automatic landing of an aircraft was designed with the methods of feedback linearization and improved fuzzy control
使用反饋線性化與改進的模糊控制方法設計飛機縱向自動著陸控制系統。Finally, system is simulated, and the results can satisfy the requests value of the aircraft landing system and it represents a strong robustness of aircraft landing control system
然後設計了自動著陸控制系統控制律,並進行了模擬,模擬結果滿足飛機自動著陸各項指標要求,表明所設計的自動著陸控制系統具有較強的魯棒性。Adaptive inverse control is applied in the design of automatic landing system and robustness is verified. good simulation results are obtained. at last, nnai is contrasted with the system adopting fuzzy control after linearization
本文以某國產飛機為對象,採用自適應逆控制的方法,設計飛機縱向自動著陸控制系統並模擬,還對所設計的系統進行了魯棒性驗證模擬。分享友人