著陸方法 的英文怎麼說

中文拼音 [zhāoliùfāng]
著陸方法 英文
landing concept
  • : 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)
  • : 陸數詞(六的大寫) six (used for the numeral 六 on cheques, etc. to avoid mistakes or alterations)
  • : Ⅰ名詞1 (方形; 方體) square 2 [數學] (乘方) involution; power 3 (方向) direction 4 (方面) ...
  • : Ⅰ名詞1 (由國家制定或認可的行為規則的總稱) law 2 (方法; 方式) way; method; mode; means 3 (標...
  • 著陸 : landing; land; touch down
  • 方法 : method; means; way; technique; process; procedure; plan; device; recipe; fashion; tool; maneuver
  1. Emphatically, this paper discusses the pattern of signal and antenna radiation of the system, the design principles and technologies of audio - generator and monitor, and the modification of measurement deviation. through special tests and aviate experiments, it has been proved that the performance of the domesticalized system is better than of the initial system

    文中重點分析了俄制分米波儀表系統的信號格式和天線輻射場型,重闡述了系統中音頻信號產生器和監測器的設計原理和實現技術,對信號檢測中的測量誤差進行了分析並設計了有效的修正
  2. Establishing an human spine dynamic model is an significan event to study spine injured biomechanics of pilot " s ejective injury, parachute opening, landing and study the endurance to impact loading on human spine. in this paper, the huston " s method of kane " s equations is developed so that it can be applied to the multibodysystem including translation between the bodyies. the dynamic model of human spine is provided basing on these theories, while the big movement of spine is considered. the deformation of vetebra is far smaller comparing with the intervetebra disc, so the spine is considered into multibodysystem including rigid bodies ( vetebra ) and the flexible bodies ( intervetebra disc ). the computer solution correspond with the results of the large scale human impact test. the rigid coefficient factors and the damping factor of intervetebra joints are obtained

    人體脊柱動力學模型的建立對研究飛行員彈射救生、傘兵跳傘開傘、等脊柱損傷的生物力學以及研究人體脊柱耐受沖擊載荷的極限問題都具有重要意義.首先發展了凱恩程的休斯頓,使其可應用於變形體連接的多體系統,並以此理論為依據建立人體整椎脊柱沖擊動力學模型,此時考慮脊柱的大位移運動,每個椎骨的變形相對椎間盤的變形小得多,把脊柱看成由剛體(椎骨)和變形體(椎間盤)組成的多體系統.並以大型真人坐姿沖擊實驗結果進行了擬合,最後得到腰椎間關節剛度系數因子和阻尼系數因子
  3. The method can eliminate the conventional fuzzy control system ' s steady - state errors and flutters. and, the method of forward feed control is used to reduce the tracing errors during glide slope phase

    在此基礎上,採用帶優化修正函數無量化的模糊控制,設計飛機的微波控制系統,並進行了閉環模擬。
  4. This article contains three parts, namely, preface, body and conclusion. the preface mainly introduces the discussing subject and writing purposes of this article. body is divided into four parts : from the beginning of actio in rem and actio in personam in roman law, the first part detailedly inspects and analyses the formation process of the dual rights system in historical research methods ; the second part discusses the theoretical framework of the dual rights structure from the aspect of system ; the third part mainly analyses the middle rights and the integration of real rights and creditor ’ s rights and the reasons for the emergence of these phenomena, pointing out that the emergence of these phenomena is unevitable in civil law system which ajusts social relationship with systematic code, and how

    正文分為四個部分:第一部分採用歷史研究的,從羅馬上的對人之訴和對物之訴出發,對物債二分體系的形成過程進行了細致的考察和分析;第二部分從體系化的角度討論了物債二分體系的理論構成,對其理論架構進行了總體上的研究;第三部分重分析了物權與債權的融合和中間狀態及其出現這些現象的原因,指出在運用體系化的調整社會關系的過程中,出現物權和債權中間狀態的權利形態是不可避免的現象,並對如何正確看待這些問題進行了論證;第四部分在前文論述的基礎上,對我國一些學者提出的制定財產和設立財產總則的觀點的可行性進行了分析,指出無論是從我國大系的傳統還是從技術層面來看,制定財產或設立財產總則都是不可行的。
  5. Based on the investigation and research, the paper gives a testing method, which measures the taking off and landing distance of airplanes with the laser locating system for airplanes trace. and by way of the field measuring on plateau airports, we have got the integrated modifying coefficients of three kinds of airplanestaking off and landing running distance such as h6. all of these provide scientific basis for the runway length design of the plateau airport

    在調研論證的基礎上,提出了利用《飛機起落航跡激光定位系統》測定飛機起飛滑跑距離的測試,並通過高原機場實地測試,得出了三種飛機在高原機場上起飛滑跑距離的綜合修正系數值,為高原機場跑道長度設計提供了可靠的理論依據。
  6. The method of wing shape optimization of space shutlle has been developed with penalty function approach in which the objective function is the mass of the wing and the constraints are the hypersonic re - entry flight cross range, lift / drag ratio, and subsonic flight lift / drag ratio, the margin of the longitudial static stability and the magnitude of the horizontal landing speed etc

    摘要介紹了在滿足高超音速再入橫向機動航程,高超音速再入飛行時的升阻比,亞音速進場飛行時的升阻比,縱向靜穩定性裕度和水平速度等飛行性能設計要求下,用罰函數尋求使航天飛機機翼質量為最小的外形優化並給出了算例。
  7. The way of inquiry is based on some classic translations, which were formally published in china and were written by the great thinker, philosopher, sociologist, scientist, or historian of science

    研究的,主要是解讀在中國大正式出版的、在西學術界享有較高聲譽的一些思想家、哲學家、社會學家、科學家以及科學史家的中文譯
  8. With the supports of lunar exploration pre - research program “ lunar soft landing integrative simulation and validation technique ”, this dissertation performed deep and systemic study on lunar explorer autonomous navigation and control issues. the main contents of this dissertation are as follows

    本文結合月球探測工程二三期預研項目「月球軟綜合模擬演示驗證技術」 ,對月球探測器的自主導航與控制進行了較深入的研究。
  9. The simulation results show that the feature point detection and tracking algorithm is feasible. next, matched points based essential matrix estimation is studied. the spacecraft attitude and position parameters are derived from essential matrix and the scale of motion is recovered with range information from laser ranger taken in account

    再次,研究基於匹配特徵點對的本質矩陣的估計演算,給出了由本質矩陣求取空間探測器的姿態信息和位置信息的,並且結合激光測距儀信息,得到探測器的運動比例參數,實現軟過程的導航。
  10. 3. edge detection and threshold segment are used in safe landing area choice

    3 .採用邊緣檢測和閾值分割進行軟安全區域選取。
  11. Fortunately, the accident was not fatal for our crew and they were able to get the plane on the ground. unfortunately, it apparently was fatal for the pilot of the chinese plane and i regret that

    所幸的是,這起事故沒有造成我們機組人員的生命損失,他們設使飛機。不幸的是,這起事故顯然造成中飛機駕駛員的死亡,對此我感到遺憾。
  12. In this paper, the method vision - based for uav autonomous landing is researched using technology of image processing, computer vision and projection geometry. the first task of computer vision - based uav autonomous landing is to recognize and track the runway using computer vision. a simple method is discussed to recognize and track the runway in the image sequences using template matching

    本文的研究工作來源於「 973 -無人作戰飛機系統」項目,以某型無人機試飛過程中拍攝的場景圖像為基本研究材料,綜合利用了圖像處理技術、計算機視覺技術、射影幾何學等研究了跑道識別與跟蹤、進場段的圖像處理、無人機段飛行參數提取等相關問題。
  13. 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的原理與特點的基礎上,將神經網路與自適應逆相結合,重研究了將這種應用於非線性系統的控制問題,最後,用飛機自動的過程,驗證了神經網路自適應逆的效果。
  14. China is petroleum production country where the oil is mainly produced in continental hydrocarborn - bearing basin. it is special feature of contineutal oil - gas - bearing basin that sandstone lithologic reservoir with variety lithologic sandbody and vely enriching rolk oil hides extensively exsited. in the center region of continental lake basin sedmentary region, rf s very difficult to predict and descript turbidite reservoir because of the special subtle of turbidite sandbody. therefore studing the sediments character of turbidite reservoir and the description methord of turbidite reservoir has the important and realistic meaning for the explore and development of turbidite reservoir

    中國是一個以相含油氣盆地為主的產油國,在相湖盆的沉積中心地區,廣泛存在以各類濁積砂體為主要儲集體且儲量相當豐富的砂巖巖性油藏,構成相含油氣盆地的一大特色。由於濁積砂巖體的特殊隱蔽性,給濁積巖儲層預測和描述帶來了很大困難。因此,研究濁積巖儲層的沉積特徵和濁積巖油藏的描述對于濁積巖油藏的勘探開發具有重要的現實意義。
  15. Finally, a new fresh concept of indirect offence is put forward on the basis of differentiating, analyzing and commenting traditional ideas of indirect offence. part this part discusses the property of indirect offence. this part begins with the introduction to various ideas about the property of indirect offence and then makes comments on each of them

    本部分首先介紹了關于間接正犯的正犯性的各種觀點,並對相關觀點一一評價,然後立足於中國大犯罪構成要件,眼于實行行為,根據主觀與客觀相統一的原則,從利用者與被利用者兩個重論述了間接正犯的正犯性。
  16. For the lunar landing phase mission, this paper presents autonomous navigation scheme based on feature points ( fps ) tracking

    針對軌道段任務,給出了一種基於特徵點跟蹤的自主導航
  17. Because of the rotation and revolution of the earth and the moon, and the variety of opposite geography position between lunar rover and earth station brought by them, sometimes the lunar rover will be placed in district which is beyond control of the earth station, so the wandering explorer make use of the metering equipment that the itself takes to carry on control and navigation independently have already become an important development direction

    月球車通常藉助地面站通過無線電測控進行導航控制,但由於地球和月球自轉和公轉運動及所帶來的地面站和漫遊車相對地理位置的變化等,有時月球車會處于地面站無測控的區域內,因此漫遊車利用自身或者器攜帶的測量設備進行自主導航控制已經成為重要的發展向。
  18. Currently chinese scholars have not deeply researched thinking foundation of continent legal system criminal theory system. according to this situation, the author tries to question continent legal system criminal theory system for contributing chinese criminal law theory and rule of law in china. this dissertation falls into eight parts

    系注重抽象的體系思考,設想建構「開放的刑體系」 ;作為體系思考對立物的問題思考以論題學為論;眼于問題解答的體系是問題的體系;犯罪要件作為問題解答工具在司實踐中被運用
  19. 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來設計非線性飛機模型自動全面控制系統。
  20. Secondly, an algorithm of image processing is introduced which can detect horizon of airfield and edges of runway commendably. and then, based on work of former researchers, it is developed which is a software system of uav ’ s autonomous landing image processing and parameter - obtained. a corresponding simulation experiment has been done making use of this software

    本文所研究的跑道的識別和跟蹤、地平線和跑道邊緣的提取、無人機飛行參數求解構成了基於計算機視覺的無人機自主著陸方法研究的主要內容,為實現相應的工程應用打下了基礎,具有重要的意義。
分享友人