進行著陸的 的英文怎麼說

中文拼音 [jìnhángzhāoliùde]
進行著陸的 英文
earthbound
  • 進 : 進構詞成分。
  • 行 : 行Ⅰ名詞1 （行列） line; row 2 （排行） seniority among brothers and sisters:你行幾? 我行三。where...
  • 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）
  • 的 : 4次方是 The fourth power of 2 is direction
  • 進行 : 1 （開展） be in progress; be underway; go on 2 （從事） carry on; carry out; conduct; make 3 （...
  • 著陸 : landing; land; touch down
  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著陸系統的信號格式和天線輻射場型，著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方法。
  2. On the basis of the research on the arresting behavior of the carrier aircraft, the arresting model of the continental rise aircraft as well as its motion analysis is presented in the paper

    本文對飛機著陸攔阻的技術進行了較深入的研究，主要是針對陸基飛機，借鑒艦載飛機的攔阻特性進行了攔阻鉤的建模及其運動學分析。
  3. 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、著陸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.首先發展了凱恩方程的休斯頓方法，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
  4. 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方法，設計飛機的微波著陸控制系統，並進行了閉環模擬。
  5. 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方法，從羅馬法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;第三部分著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方法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法和設立財產法總則的觀點的可行性進行了分析，指出無論是從我國大陸法系的傳統還是從技術層面來看，制定財產法或設立財產法總則都是不可行的。
  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著陸速度等飛行性能設計要求下，用罰函數法尋求使航天飛機機翼質量為最小的外形優化方法並給出了算例。
  7. After an elementary study with lunar orbiting satellite, it is necessary to make exploration devices land on the moon and carry out detailed exploration with lunar rover in a rather large area

    在利用環月衛星對月球進行初步的探測之後，需要使探測器在月球表面軟著陸，並由月球車執行較大范圍的詳細探測任務，為載人登月和建立月球基地做好準備。
  8. The state ( or region ) of the aerodrome has to provide data such as obstacle clearance altitude height ( oca h ), details of electronic aids for an approach to landing, etc, to enable an operator to establish aom for each runway intended to be used at that particular aerodrome

    機場所屬國家或地區須提供資料，例如：超障安全高度、協助進場著陸的電子輔助設備的詳細資料等，使營運人能夠就某個機場內擬使用的每條跑道確立機場最低飛行條件。
  9. Under the analysis of a great deal of civil aviation accident, this command assistant system is brought forward which aimed to lowed the ratio of approach and landing accident reduction

    通過對大量民航飛行事故的分析，提出了一種旨在降低進近著陸過程事故率的輔助指揮系統。
  10. Aom tells very instrument pilot under what visibility ( in terms of runway visual range ( rvr ) ) and or cloud ceiling can the aircraft take off, and under what visibility ( again in terms of rvr ) and visual reference can the aircraft continue the approach to land from the decision altitude ( for precision approaches, e. g. instrument landing system ( ils ) ) or from the minimum descent altitude ( for non - precision approaches ). there are a number of factors affecting the values of aom

    機場最低飛行條件讓每名按儀表駕駛的飛行員知道，航空器在什麼能見度以跑道能見距離來說及或雲幕高度下才可起飛；以及航空器在什麼能見度以跑道能見距離來說及目視基準下，才可從決斷高度用於如使用儀表著陸系統的精確進場或最低下降高度用於非精確進場繼續進場著陸。
  11. A large planar microphone array, which consists of 111 microphones, was successfully applied to obtain a two - dimensional mapping of the sound sources on a landing aircraft. the focus of study in this paper is on the landing gear noise source. the spectra, directivities and sound pressure levels of flap side - edge noise of 7 narrow - board commercial aircraft and 7 wide - board commercial aircraft are presented. it is found that the landing gear noise spectrum is broadband with some single tones in some cases. the directivity of the total sound pressure level of a landing gear noise resembles that of a horizontal dipole. the level differences between the various aircraft landing gears are larger than those expected from the airspeed differences. it is thus expected that the louder noise emission of the landing gears can be reduced by redesigning

    應用由111個傳聲器組成的平面傳聲器陣列對當前流行的民用客機進場著陸過程中的機體噪聲源進行了實驗測量，本文對七架窄體客機和七架寬體客機的起落架噪聲進行了分析，得到了起落架噪聲的頻譜特性、指向特性和聲級變化.研究發現，起落架噪聲的頻譜是由寬頻隨機噪聲與一些較為明顯的單音噪聲源組成，起落架噪聲的指向性類似於一個水平放置的偶極子.不同飛機起落架噪聲的聲級相差較大，這說明可以通過重新結構設計降低起落架噪聲。
  12. Reference the fsf ' s landing hazard consciousness checklist, the pre - take - off hazard consciousness checklist was elicited to improve the scene consciousness. several representative accident that happened in our country and the effect of crm, approach procedure, airborne equipment and approach environment to the flight safety was analysed

    進近著陸事故分析中，分析了我國幾起典型的進近著陸事故原因，又分別從機組資源管理、進近程序、機載設備、進近環境等方面對飛行安全的影響進行了分析研究，並列出了國際飛行安全基金會提出的進近著陸風險意識檢查單。
  13. 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著陸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、射影幾何學等方法研究了跑道識別與跟蹤、進場著陸段的圖像處理、無人機著陸段飛行參數提取等相關問題。
  14. Abstract : a large planar microphone array, which consists of 111 microphones, was successfully applied to obtain a two - dimensional mapping of the sound sources on a landing aircraft. the focus of study in this paper is on the landing gear noise source. the spectra, directivities and sound pressure levels of flap side - edge noise of 7 narrow - board commercial aircraft and 7 wide - board commercial aircraft are presented. it is found that the landing gear noise spectrum is broadband with some single tones in some cases. the directivity of the total sound pressure level of a landing gear noise resembles that of a horizontal dipole. the level differences between the various aircraft landing gears are larger than those expected from the airspeed differences. it is thus expected that the louder noise emission of the landing gears can be reduced by redesigning

    文摘:應用由111個傳聲器組成的平面傳聲器陣列對當前流行的民用客機進場著陸過程中的機體噪聲源進行了實驗測量，本文對七架窄體客機和七架寬體客機的起落架噪聲進行了分析，得到了起落架噪聲的頻譜特性、指向特性和聲級變化.研究發現，起落架噪聲的頻譜是由寬頻隨機噪聲與一些較為明顯的單音噪聲源組成，起落架噪聲的指向性類似於一個水平放置的偶極子.不同飛機起落架噪聲的聲級相差較大，這說明可以通過重新結構設計降低起落架噪聲。
  15. From the simulation, we can get some parameter curves of landing gear. by analyzing these curves and the methods with two - masses model, the linear state equation of landing gear during landing process was established

    基於參數曲線分析和二質量模型建立了起落架著陸的線性狀態方程，應用現代控制理論對方程進行分析並結合matlab軟體對其進行著陸動態模擬。
  16. So approach - and - landing ( eight minutes ) is one of the most important phase to which aircraft liable occur serious accident, civil aviation people regard them as " dangerous eight minutes "

    因此進近著陸（ 8分鐘）是航空飛行器最容易發生重大事故的階段之一，民航人將其視為「危險的8分鐘」 。
  17. At the same time, the altitude and dynamic pressure are also controlled by kernel extraction protocol equations of motion to satisfy the requirements of autolanding

    同時利用kep運動方程對高度和動壓進行控制，以便滿足自動著陸的要求。
  18. 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。
  19. He had heard that the people in mainland china have changed a lot in recent years, and more and more people are seeking spiritual growth at various levels. he was confident that supreme master ching hai s teachings would be of benefit to his friend. the display booth for supreme master

    因為他聽說中國大陸的人們近幾年有了許多變化，越來越多的人在不同的層面，進行著精神和靈性的追求，清海無上師的教理一定會對他的朋友有所幫助。
  20. The sehk, hkma and hkscc believe that the listing will boost the development of the local bond market by paving the way for similar listings by other public and corporate issues

    聯交所金管局及香港結算均深信，在外匯基金債券上市后，其他的公共機構及公司當會陸續進行類似的上市活動，對本地債券市場的發展起著極大推動作用。
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