landing-gear control 中文意思是什麼

landing-gear control 解釋
起落架收放
  • landing : n. 1. 登陸；著陸，降落；下車。 2. 登陸處；（飛機）著陸地；碼頭；（車站的）月臺。3. 【建築】樓梯平臺；梯臺；【林業】集材場，貯木場；【礦物】裝卸臺。4. 【無線電】（電子的）沉陷，沉澱。
  • gear : n 1 【機械工程】齒輪，（齒輪）傳動裝置，齒鏈；排擋。2 〈古語〉衣服；甲胄與武器。3 傢具；財物，動...
  • control : n 1 支配，管理，管制，統制，控制；監督。2 抑制（力）；壓制，節制，拘束；【農業】防治。3 檢查；核...
  1. One night, she and fred were flying in their twin engine cessna skymaster when the landing gear couldn t be lowered. adella was not afraid to live. she was not afraid to die. so she was in control over her emotions

    有一次他們的小型飛機的降落架沒有降下來，當時不是她駕駛，她不怕活著，她不怕死亡，她很能控制自己的情緒，當費特說：雅德，降落架沒有降下來，那就是說我們要緊急降落。
  2. In this paper, the mathematics model and simulation model of the passive landing gear shock absorber was built, and was verified by drop test. aimed at acquiring suitable efficiency diagrams, two simple semi - active control algorithms were designed. the mathematics model and simulation model of the semi - active landing gear shock absorber was built

    在本文中，建立了被動控制起落架緩沖系統數學模型和模擬模型，並通過落震試驗對該模型進行參數校驗；以合適的功量圖為控制目標設計出兩種半主動簡單控制律，建立了半主動控制起落架緩沖器數學模型和模擬模型；通過數字模擬對這兩種控制方法進行了比較，認為半主動控制較被動控制有很大的優越性。
  3. This paper mainly researches the application of the active control technology to the landing gear system. the aim is using different control methods to design the active controller to improve the performance of the system, according to the characteristic of the parameters " variations

    本文主要研究了主動控制技術在起落架緩沖器控制系統中的應用，針對緩沖器系統變參數的特點，運用不同的方法來對主動控制器進行了設計，達到了改善系統性能的目的。
  4. Simulation results shows that adaptive control algorithm can make the output of aircraft landing gear approach to the reference output rapidly and the control system possess of good performance of robustness. hence, the control method is effective

    模擬結果表明:自適應控制演算法能夠使起落架的控制變量快速達到理想的參考模型輸出並且控制曲線平滑，同時控制系統具有很好的魯棒性能，增強了系統的抗干擾能力。
  5. Simulation shows : the linear model can explain the characteristic of the passive control landing gear

    結果表明線性化后的模型能夠反應被動控制起落架的著陸特性。
  6. There are three control methods of aircraft landing gear : passive control, active control and semi - active control

    對起落架的控制方法經歷了被動控制、主動控制和較新的半主動控制三個過程。
  7. In general, the control methods of the aircraft ' s landing gear shock absorbers are classified three categories : a passive type, an active type, and semi - active type

    一般地說，飛機起落架緩沖系統的控制方式有三種：被動控制、主動控制和半主動控制。
  8. Intelligent semi - active control landing gear for flexible airplane

    柔性飛機起落架智能半主動控制
  9. The research and discussion presented in this paper are semi - active control technology applied on the aircraft landing gear

    本文對半主動控制技術在起落架上的應用做了研究和探討。
  10. The development of semi - active control technology and the equipment : magnetorhelogical fluids damps based in this technology were introduced. the discussion presented in this paper is this equipment applied on the aircraft landing gear

    本文分析了半主動控制技術的發展概況並構建了磁流變阻尼器，並對其在飛機起落架上的應用作了進行了初步探討。
  11. Among them, as a compromise between active control and passive control, the controllability of semi - active control is access to full active control, and in the same time, the method is simpler, lighter and safer than full active control. it ' s suitable for the applications in landing gear shock absorbers

    其中半主動控制介於被動控制和主動控制兩者之間，具有類似主動控制的可控性，同時具有結構簡單、重量輕、安全性高的特點，適合於在起落架緩沖系統中的應用。
  12. Some effective methods are given out to eliminate the extra force in this paper, such as variable structure pid control, position compensation, and velocity feedback. they greatly improve the performance of the loading system. but for the full - loading of fore - landing gear, it still ca n ' t meet the loading precision completely

    為了克服多餘力，本文採用了變結構的pid控制及位置補償、速度反饋等方法，對于主起全載和前起半載試驗，取得了良好的效果；而對於前起全載試驗，在進一步採用對給定載荷譜進行濾波，模糊控制等方法后仍不能完全滿足要求的性能指標，在加載試驗研製總結中簡單分析了其原因。
  13. The application of adaptive control in aircraft landing gear is an important innovation to modern airplane design

    自適應控制在飛機起落架的應用是一個比較新的課題。
  14. Another way to attenuate the landing impact loads is to embed a control system into landing gear system

    對飛機起落架在降落區上著陸的情況進行了數值模擬分析並做了相關參數研究。
  15. The paper mainly discussed and analyzed aircraft landing gear using model reference adaptive control and mcs ( minimal control synthesis algorithm ), built up the mathematics model and linear state equations of aircraft landing gear during the landing and taxiing and analyzed the virtues of model reference adaptive and minimal control synthesis algorithm

    本論文主要是採用模型參考自適應和最小控制綜合演算法（ minimalcontrolsynthesisalgorithm ）來描述飛機起落架系統，建立了完整的起落架著陸滑跑的數學模型和線性狀態控制方程，分析了模型參考自適應和最小控制綜合演算法的優點。
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