飛行實驗 的英文怎麼說

中文拼音 [fēihángshíyàn]
飛行實驗 英文
flight experiment
  • 飛 : Ⅰ動詞1 （鳥、蟲等在空中活動） fly; flit 2 （利用動力機械在空中行動） fly 3 （在空中飄浮遊動） fly...
  • 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...
  • 實 : Ⅰ形容詞1 （內部完全填滿 沒有空隙） solid 2 （真實; 實在） true; real; honest Ⅱ名詞1 （實際; 事實...
  • 驗 : 動詞1. （察看; 查考） examine; check; test 2. （產生預期的效果） prove effective; produce the expected result
  • 飛行 : flight; flying; aviate; voyage; volitate; hop
  1. This research work on bird striking has a long history and already got plentiful achievemellts in theories and experiments, howevef, still a long way no doubt waits to go for sophisticated research work on it more detailed to apply to airframe engineering quantitatively in combination wth the technical reformation of the birdstrike experimelltal system in our laboratory, this thesis deeply studies and analyses the numerica1 computation and simulation methods to birdstrike dynamic response problem based on finite - elemefit - method ( fem ) numerical emulation and modem large - scale scientfic computation software

    本文結合我公司鳥撞實驗體系技術改造項目，應用有限元數值計算模擬技術及現代大型科學計算工具，對鳥體撞擊飛機風擋結構的動力學響應問題進行了系統學習與研究探討，初步掌握了科學計算方法，獲得了計算模擬的實踐經驗，為今後深入應用大型科學計算手段進行撞擊類科學問題的研究以及深入應用於工程實踐奠定了強有力的工作基礎。
  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、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
  3. Terrans have different add - ons for their buildings, ( 1 ) is laboratory for factory, ( 2 ) is reactor for barracks. " flyable " buildings can switch their add - ons

    人族建築擁有不同掛件， （ 1 ）是重工場的實驗室， （ 2 ）是兵營的反應堆。能飛行的建築可以轉換不同的掛件。
  4. Application the retrieval coefficients of the city of changchun in april to a field experiments in jilin province, on april 22 demonstrate the airborne up - looking microwave radiometer can detect cloud liquid water and supercooled liquid water content

    此外，本文將求得的長春地區4月的反演系數應用到長春4月22日的一次飛行實驗中，結果表明，能夠探測出雲中液態水和過冷水含量及其變化。
  5. This paper analyses the applied characteristic of phase - locked loops ( pll ) for the forward motion compensation technology of lmk aerial survey camera. according to the analysis, a new style pcb is produced. the realization by software for the forward motion compensation is discussed in this paper, which is realized by the ti prduction tms320f240

    在對lmk航空攝影機像移補償控制系統的再設計工作中，本人設計出了新的補償電路線路板，並進行了幾項典型的實驗研究和前向運動補償效果評價，經過外場飛行試驗，進一步證明了該設計的可靠性、可行性、實用性。
  6. It has been maked for immediate and statistical analysis that the calculation about the work order parameter of the base - bleed - rocket is calculated in the taguchi method, its influencing trend is bring out in the open, the theoretical base is settled for confirming the greatest combination about the work order parameter of the base - bleed - rocket. the multi - objectile optimal design model is established that the indexes have been taked into account first and synthetically, such as physical parameter range lethality power strength and flight stability and so on, the program is compiled and the example is calculated. the true worth of the theoretical work in this paper is validated by flight experimentation of 130mm hybrid base - bleed - rocket extended - range principium projectile

    本文進行了底排?火箭復合增程彈工作時序參數正交試驗設計的直觀分析與方差分析，揭示了每個參數對射程計算的影響趨勢，為進一步確定底排?火箭工作時序參數值的最佳匹配組合奠定了理論基礎；建立了底排?火箭復合增程彈多目標優化設計模型，該模型首次綜合考慮了底排?火箭復合增程彈的結構特徵參量、結構強度性能、飛行穩定性、威力性能和射程指標，編制了相應的分析程序，進行了算例計算；完成了130mm底排?火箭復合增程原理樣彈的結構設計與飛行試驗，其試驗結果驗證了本文理論研究工作的實際應用價值。
  7. Then a low pass filter is designed to filter high - frequency noise in data. and smooth data again by means of central interpolation algorithm ; helicopter model with multi input single output are identified respectively in ls method and ml method

    （ 2 ）剔除並補正了飛行實驗數據中的野值；設計了一個低通濾波器來濾除數據中的高頻噪聲；用中心插值演算法對數據二次平滑。
  8. In conclusion, the paper regards that the developing direction of adopting simulation technology for the test and evaluation of guided weapons is setting up the all - around test and evaluation mode that real test conjoins hitl simulation test

    得出結論認為，建立實際飛行試驗與半實物模擬試驗相結合的綜合試驗模式，是模擬技術在制導兵器試驗與鑒定中應用的發展方向。
  9. The results of flight test show that this multi - sensor integration technology can ensure the reliability of flight control system, and realization of a bvr ( beyond the visual range ) and high precision autonomous flight control

    通過飛行試驗表明，多傳感器的信息綜合技術能夠保證飛行控制系統工作的可靠性，實現超視距、高精確度自主飛行控制。
  10. Monitoring the change will give us useful information about the sample. the paper begins from analyzing the principle of ecndt, studies the feasibility of the clearance detection between two metal plates using eddy current, furthermore makes experiment research

    本文結合我國某飛機工業集團公司的《飛機蒙皮貼胎間隙檢查儀方案設計》研究項目，研究了渦流技術在多層金屬板厚度或板間間隙檢測的可行性，並進行實驗驗證。
  11. In consideration of the special mission characteristics and technical requirement of high altitude long endurance unmanned aerial vehicle, an authentic real - time and space - time windfield integrated model is accomplished to take atmosphere environment influences into account. at the same time, we should analyze the dynamics the uav encounters dispersedly, so the " finite scale " aircraft concept is quoted

    根據長航時無人機的特殊飛行任務特點和技術要求，在飛行試驗階段，有必要綜合考慮飛行環境中各種大氣干擾因素的影響，為無人機設計與模擬提供一個真實、適時的風場時空分佈模型。
  12. The thesis is composed of three parts, i. e. model choice, experimental data preprocessing, and parameters identification

    論文主要包括辨識模型選取、飛行實驗數據預處理和參數辨識三部分。
  13. The memory mapping technology and multithreaded i / o operation of scsi processor is applied to the design of real time storage system

    將內存映射和scsi處理器多線程f o調度技術應用到實時存儲系統的設計中，獲得實驗室和飛行實驗的實驗數據。
  14. Shenzhou 5 single - astronautic, one day and shenzhou 6 multi - astronautic, is the great landmark in our aerospace technology, which indicating the maturity in this field

    神舟5號首次載人航天和神舟6號多人多天的飛行實驗成功是我國航天事業的一個重大里程碑，標志著我國航天技術的不斷成熟。
  15. With amounts of flight experiment, proved the design could satisfy the demand of large quantities of data in down channel and high precision and reliability of control parameters in up channel

    經大量完全自主飛行實驗結果表明，所設計的監控系統軟體不僅能夠滿足小型無人機下行通道傳輸數據量大的監測要求，而且可以確保上行通道控制參數高精度、高可靠性的要求。
  16. The relationship between the load measured by strain method and the load calculated according to flight parameters and the wind tunnel test data has been investigated in this thesis. the result showed that the calculation load based on the flight parameters and wind tunnel test data is acceptable in subsonic speed and gets good agreement, with the load measured by strain method

    本文研究了採用應變法實測載荷和根據飛行實測參數和風洞實驗數據計算載荷之間的關系，研究表明採用飛行實測參數和風洞實驗的數據計算載荷在亞音速范圍內是可行的，與採用應變法實測載荷是吻合的。
  17. In the flight experiment of aircraft, the mass data acquisition, storage and transfer is always one important part of system, especially for the measurement of parameters such as temperature and pressure of cockpit. in order to meet these needs, we design this simultaneous data acquisition system with multi - channel and large - capacity, which is based on single chip microprocessor and usb interface. it overcomes some shortcomings of traditional devices such as : big size, short work time, small memory capacity etc. it also has many advantages of high speed, low power dissipation, ease - of - use, ease to expand port, supporting plug - play, low - cost etc, so it will be used very widely

    在飛機的飛行試驗中，海量數據的採集、存儲和傳輸一直是系統非常重要的一部分，尤其是對飛行員駕駛艙環境控制系統的溫度、壓力等參數的測量來說更是如此。本文根據課題實際需要，研製的基於單片機和usb介面的多通道、大容量、便攜式數據採集系統，克服了現有設備體積大、工作時間短、存儲容量小等缺點。同時，本系統還具有功耗低、速度快、使用方便靈活、易於擴展、支持即插即用、成本低廉等一系列優點，具有廣泛的應用前景。
  18. After practicing the strategic decision, by oct. 15th 2003, important flight tests succeed for 30 times. shenzhou v realized chinese first man - carrying flight. these show the fruits of strengthen the management of scientific research and manufacture and testify its right efficiency and holds and the essential of the problem

    戰略決策實施之後，截止2003年10月15日，重大飛行試驗連續30次取得成功，神舟五號順利實現中國人的首次載人航天，展示了實施強化科研生產管理的成果，證明實施這一戰略決策是正確的、有效的，抓住了問題的實質。
  19. Save, query and graphic interaction dealing with the result of actual flight test data are the emphasis of flight test database

    飛行試驗數據庫的側重點在於對實際飛行試驗結果數據的存儲、查詢和圖形化處理。
  20. Firstly, total system could be divided into four parts including simulation algorithmic library, simulation knowledge library, flight test database, simulation test database, according to characters of resources and functional differences of flight simulation, and then these parts are designed and accomplished respectively

    首先，根據飛行模擬資源的特點和功能上的區別，可以將整個系統從總體上劃分為模擬演算法庫、模擬知識庫、飛行試驗數據庫和模擬試驗數據庫等四個部分，然後分別進行設計和實現。
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