test landing 中文意思是什麼

test landing 解釋
研究性著陸
  • test : n 1 檢驗，檢查；考查；測驗；考試；考驗。2 檢驗用品；試金石；【化學】試藥；（判斷的）標準。3 【化...
  • 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。
  1. 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
  2. Test and analysis of airplane ' s running track in taking o ff and landing

    飛機起飛著陸航跡測試與分析
  3. Standard test method for characterization of gymnastic landing mats and floor exercise surfaces

    體操用著地墊和訓練用地板面特性的標準試驗方法
  4. Gymnastic equipment - parallel bars with landing mat between the frame - requirements and test methods ; consolidated version with din en 914

    體操器械.帶墊子雙杠.要求和試驗方法
  5. 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。
  6. The landing test included overhead approaches as well as straight in approaches from normal, high, low, and laterally offset starts

    著陸測試包括：高空、低空、正常狀態以及橫向偏置狀態的轉彎進場著陸和直接進場著陸。
  7. This system included the following modules, such as registration landing module, students course selecting system, resources browsing and downloading, off - line work, on - line test and result inquiry, study behavior record, auto - answer ; the teacher resource management, the off - line work management, the on - line test management, the on - line statistics ; the manager took the responsibility of the personnel management, the resource

    本系統包括了注冊登錄模塊、學員選課系統、資源瀏覽和下載、離線作業、在線測試與成績查詢、學習行為記錄、自動答疑;教師資源管理、離線作業管理、在線測試管理、在線統計;管理員進行人員管理、資源管理、權限管理、課程計劃管理;另外還有教學討論、實時答疑、個人信息維護、收藏夾、記事本、通訊錄等模塊。
  8. By the test system of the landing ladder on the earth which releases by an elastical structure, measure the acceleration of the ladder in the chosen directions in the process of releasing

    最後，加工著陸梯和實驗平臺，搭建合理的測試系統。對彈出式著陸梯在地面環境進行釋放試驗，觀察著陸梯釋放的情況，測量著陸梯彈出過程中選定方向的加速度。
  9. Aircraft assembling technology assembling ang test for landing gear

    飛機裝配工藝.起落架的裝配與試驗
  10. The work involves : 1 based on the analysis of previous ddm schemes, considering source - based, destination - based, intermediate filtering mechanism, this paper gives clearly reason and excellence of selecting light - weight mode architecture ; 2 the paper displays light - weight ddm scheme in details, including the relationship of ddm service with other services and object attributes, relevant element designment and algorithm designment ; the paper analyses information flow in light - weight ddm scheme, dividing all implementing classes of ieee 1516 interface specification, showing ddm federate process and explaining how to use " infantry division landing island joint warfare simulation system " to test all ddm implementation algorithms

    這主要包括： 1 、在綜合分析ddm所有實現方式的基礎上，包括基於agent 、網格和區域等實現方法，結合源端、中介端、目的端過濾機制，首次提出了ddm弱服務器模式體系結構； 2 、論文首次給出ddm弱服務器模式方案的具體設計，包括ddm與聲明服務、對象服務、所有權服務、時間服務及與對象屬性的關系，相關基礎設計和詳細演算法設計等。 3 、最後，論文給出了弱服務器實現模式的信息流向，分析了ieee1516介面規范實現時用到的所有實現類，以及符合ieee1516規范的ddm成員流程，論述了利用「 xxx作戰」模擬工程綜合測試數據分發管理的過程。
  11. Safety rules for the construction and installation of lifts - examination and tests - landing doors fire resistance test

    升降機建造和安裝的安全規則.檢驗和試驗.電梯入門防火試驗
  12. Safety rules for the construction and installation of lifts - examination and tests - part 58 : landing doors fire resistance test

    電梯建造和安裝的安全規則.檢驗和試驗.第58部分:電梯入門防火試驗
  13. Safety rules for the construction and installation of lifts - examination and tests - part 58 : landing doors fire resistance test ; german version en 81 - 58 : 2003

    電梯建造和安裝的安全規則.檢驗和試驗.第58部分:電梯
  14. Esa wants the international moon programme to begin in 2002 with a 300 million - pound mission to test lunar landing techniques

    歐洲航天局希望國際月球項目能夠在2002年啟動，通過價值3億英鎊的爆炸發射來檢測月球登陸技術。
  15. Tltv. 2 : aircraft ground equipment - design, test and maintenance for towbarless towing vehicles interfaced with nose - landing gear - part 2 : regional aircraft

    飛行器地面設備.帶前起落架的無牽引桿的牽引車輛
  16. Based on the analysis of the temperature test result of the landing rectangle aqueduct of caohe river for the emergency water supply project of the beijing - shijiazhuang section on the middle route of the south - to - north water diversion project, the temperature developing feature of the early - age hydration heat of the thin - wall concrete is described, and then the main effecting factors of the hydration heat temperature on the landing rectangle aqueduct and the control measures concerned are put forward herein

    摘要通過對南水北調中線京石段應急供水工程漕河渡槽段落地矩形渡槽溫度測試結果的分析，闡述了薄壁混凝土早期水化熱溫度發展的特點，提出了影響落地矩形渡槽水化熱溫度的主要因素與控制措施。
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