飛行分析 的英文怎麼說

中文拼音 [fēihángfēnxī]
飛行分析 英文
flight analysis
  • 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...
  • 分 : 分Ⅰ名詞1. （成分） component 2. （職責和權利的限度） what is within one's duty or rights Ⅱ同 「份」Ⅲ動詞[書面語] （料想） judge
  • 析 : Ⅰ動詞1. （分開; 散開） divide; separate 2. （分析） analyse; dissect; resolve Ⅱ名詞（姓氏） a surname
  • 飛行 : flight; flying; aviate; voyage; volitate; hop
  1. Based on the frequent occurrence of international aerial crimes, the rampancy and cruelty of criminals and the reality of brutal consequence, the essay analyses the features of the crime of aircraft hijacking, the crime of imperiling international civil aerial security and the crime of obstructing international aerial navigation with the component terms from three important international conventions on punishing aerial crimes in order to help people to appreciate the appearance and the essence of typical international aerial crimes deeply, to regard the motion of the crimes and to overwhelm the offence forcefully. based on the core of the legislative status of international civil aerial security, the jurisdiction of the aerial crimes, one emphasis of the article is to clarify concrete clauses on jurisdiction in the three conventions and analyses the important principle of " aut reddere, aut punire ". based on the problems on the jurisdiction of crimes in international society, it quests the implementation of t he principles of jurisdiction, pleading and extradition in the three conventions deeply

    基於目前國際社會航空犯罪時有發生，犯罪分子猖獗狠毒，危害後果十分殘重的現實，本文從國際社會關于懲治航空犯罪的三個重要國際公約（東京、海牙、蒙特利爾公約）中規定的各種航空犯罪的定義入手，深入展開了對劫持航空器罪、危害航空器飛行安全罪、危害國際民用航空機場安全罪的犯罪特徵及其構成條件的分析，以期幫助人們更深刻認識這些典型的國際航空犯罪的表現及其實質，嚴密注視這些犯罪的動向，對其進行及時有力的打擊；鑒于國際民用航空安全法律地位問題的核心是解決航空犯罪的管轄權問題，本文重點闡釋了三個公約關于管轄的具體規定，並側重分析了「或引渡或起訴」的重要原則；鑒于目前國際社會打擊國際航空犯罪管轄方面存在諸多實際問題，本文對公約規定的管轄、起訴、引渡原則的實現方式作了深入探討；鑒于各國在國內立法上對于空中犯罪的懲治、對違約國的制裁、對這類犯罪的預防措施等方面存在一些漏洞，本文根據目前掌握的一些資料，在獨立思考的基礎上，提出了一些不成熟的看法及建議，以期對國際社會懲治航空犯罪貢獻自己微薄之力。
  2. Then, six evaluation methods ( double ratio analysis evaluation method using regional rainfall tendency control for single cloud seeding operation case, regression analysis evaluation effects on the bases of regional correlation and developing tendency of rainfall, multiple regression analysis evaluation effects on the bases of regional developing tendency of rainfall, cluster - analysis - based floating control historical regression method with uniform precipitation and atmospheric precipitable water as meteorological covariates, cluster - analysis - based floating control historical regression method with uniform precipitation used as meteorological covariate, and float ing control historical regression method ) were compared and analyzed with the case of the cloud seeding operation on 5 april 2002 in henan province

    然後，以河南省2002年4月5日飛機增雨作業為個例，對作業區域趨勢對比雙比分析評估方案、區域趨勢相關回歸分析方案、區域趨勢多元回歸分析方案、以降水量為協變量的ca - fcm方法、以降水量和整層大氣可降水量為協變量的ca - fcm方法和fcm方法6種評價方案進行分析比較。
  3. " he ' s not a sailor, he ' s a competitive sailor, " says sg cowen aerospace analyst cai von rumohr. " and that carries over to the business side.

    「他不是個水手，他是個競技型水手， 」 sg國紋飛行分析家凱?馮?如莫禾評價到： 「他將船劃到了商界。 」
  4. The condensed water separated from the air - conditioning system of an airplane is sprayed in the cold side of the radiator, and the heat transfer and the state change of water in the process of its spraying to the ram air are analyzed

    摘要將飛機空調系統中水分離器分離出的游離水噴到散熱器的冷邊，並對水噴到沖壓空氣中的狀態變化過程和傳熱過程進行分析和計算。
  5. Using this model, not only the normal static and dynamic characters of aircraft epgs but also the fault state system can be simulated. it is useful to analyse and design aircraft epgs

    利用本文開發的模型，不僅能模擬電源系統及其部件正常工作時的穩態和動態特性，而且能模擬其故障狀態，有助於對飛機電源系統進行分析和設計。
  6. This paper analysis the low using rate are armada ' s environment spectrum. for most warcraft calculate the placement spectrum is enough. the placement spectrum is composed of moist heat atmosphere, dry heat atmosphere and water solution corrode mediator soak environment

    本文對使用率較低機群的使用環境譜進行分析，總結出大多數軍用飛機使用環境譜僅需考慮停放環境譜，停放環境譜主要由大氣濕熱環境、乾熱環境和水溶液腐蝕介質浸泡環境（或鹽霧環境等）三種介質環境所組成。
  7. The performance of the system designed will directly affect the overloading that an aircraft can bear, the safe overrunning length of runway as well as the changes of tensile force of belt and braking pressure of oil, and ultimately has influence on the arresting effects. so in the process of developing a system, we should study the system in order to define the optimal configuration parameters or more effective control methods

    攔阻系統設計的優劣會直接影響到飛機承受的過載、安全攔停距離及帶拉力、剎車壓力的變化狀況，最終影響攔阻效果，因此在研製系統過程中，要對系統進行分析研究，以確定最佳的結構參數和更有效的控制方法。
  8. According to the re - attacking property of the drone using the method of zero times sample test, the loss of the drone in flight test is decreased. after the data of hitting point is gotten in test, the bayesian method, which is based on the data of the test and the information of the simulation before the test, is used to analysize the precision guidance

    對飛行試驗的靶試結果的分析，採用了兩種方法：零次靶試和小子樣靶試，零次靶試利用了無人機可拉起后進行重復攻擊的特性，以減少試驗損失，在得到落點數據后，運用bayes方法對落點信息和模擬信息進行分析，獲得其制導精度。
  9. Flyer initiation ability is evaluated by means of energy characterizing method on the basis of flyer initiation sensitivity device in the laboratory in the paper. and after theoretically calculating, utilizing gross energy in the system subtracting energy every section consuming flyer energy can be calculated finally

    本文在對實驗室建立的飛片起爆感度裝置進行分析的基礎上運用能量表徵法對飛片起爆能力進行了評價，通過對系統中各個部分消耗的能量進行理論計算，再利用系統總能量減去各個部分消耗的能量，最終得到系統給飛片的能量，進一步得到飛片撞擊炸藥時刻的速度。
  10. This thesis makes research on the n # fuel tank section of some model plane in some company with the principle and technology of work research

    本文運用工作研究的原理和技術對某飛機製造公司某型號飛機n #油箱段鉚接裝配生產線進行分析研究。
  11. Finally, this dissertation reviews the federation security and the next works need to do. in practice, this dissertation has creatively finished the following works : to derive and expand the theory and method for simulation development based on hla ; to develop the object model developing tool kd - omdt that is complied with dmso hla omt specification and will be updated to comply with ieee 1516. 2 soon ; to design and guide to implement the object model library ( oml ) shared by internet net ; to modify a large scale flight analysis and training system with hla ; to use the case tool rational rose to develop hla simulation system ; to design and guide to implement a automatic tool used to develop hla simulation with matlab / simulink

    特別地，本文在實踐中創新性地完成了以下工作：系統地提煉、擴展了基於hla進行模擬應用開發的原理與方法；開發了具有自主版權、符合dmsohlaomtv1 . 3規范的對象模型開發工具kdomdt ，向ieee1516 . 2的移植工作正在進行當中；設計並指導實現了基於internet網共享的hla對象模型庫（ oml ） ；成功地採用hla對某大型飛行分析訓練系統進行了改造；成功地將case工具rationalrose軟體應用於hla模擬系統的開發；設計並指導實現了基於matlab simulink開發hla模擬應用的自動化工具。
  12. The paper through to analyse the background, meaning and necessity for implement bidding & tender of online architectural design, through to discript and compare with different mode of domestic and international of application for bidding & tender in network, to propose a unique opinion of solution system which is ndbs mode for bidding & tender of online architectural design, the mode is to submit the whole course of bidding & tender of online architectural design from planning for bid, information issue, pre - qualification, call for bid meeting, tender submit, tender evaluation and confirm the solution to sign the contract in internet. the paper through to structure a bidding platform ( bdb. cn ), to analyse the funcation procedure of bidding and tender system of online architectural design, from the sight of bid invitor, bidder and tender evaluated angle, to link them closely. the paper carry on system design to ndbs mode, input and outut, the information and keep them, safety and data stored, the paper combine with online architectural desigh wenzhou huameng building ( railway station road 1 - 2 massif ) as an example of ndbs mode finally, the result of study indicate, bidding and tender of online architectural design is not only feasible technically, the procedure of bidding and tender accord wigh the law, but also it is unanimous in traditional bidding way, this implement the scheme can improve working efficiency greatly, reduce the cost of bidding effictives, make it standard science further, to realize a pualitative leap in the building management level

    論文通過對實施網上建築設計招標投標的背景、意義及必要性進行分析，通過對國內外不同模式招標投標網路應用的綜合敘述與比較，提出了具有獨特見解的系統的網上建築設計招標投標解決方案? ? ndbs模式，該模式是對建築設計招標投標全過程從招標準備、信息發布、資格預審、招標會議、標書遞交、評標決標到合同簽訂的網上解決方案，論文從構建網上招標平臺（ bdb . cn ）開始，對建築設計招標投標系統的功能流程進行分析，從招標人、投標人和評標人的角度出發，通過對其在整個招標投標活動流程在網際網路中的無縫連接，使得通過bdb . cn招標平臺，能夠達到建築設計招標投標各參與方的一網打盡。論文還對ndbs模式進行了系統設計，對輸入輸出、安全與數據加密和招標投標資料儲存進行設計，從技術的層面對該系統提出了解決的方案。論文最後還結合溫州華盟大廈工程（車站大道1 - 2 #地塊）的網上建築設計招標投標的實例，對ndbs模式進行了實證，研究結果表明，實施網上建築設計招標投標，不僅在技術上是成熟可行的，在工作流程上是符合法律法規的，與傳統的招標投標方式也是一致的，而且能夠大大提高工作效率，有效降低招標投標成本，使得招標投標能夠更加規范、科學，實現建設管理水平的一個質的飛躍。
  13. The target of this thesis is to develop a design and optimization tool for airfoils of wind - in - ground air vehicle. the functions of the tool include : to generate wing - in - ground air vehicle airfoil by relative less control points, to simulate the wing - in - ground effect by the mirror method, to analyze aerodynamic performance of the airfoil using the software javafoil and to optimization the airfoil by the based - surrogate optimization method

    該軟體具有如下特點:給出較少的控制點生成一個地效飛行器翼型;採用鏡像法來模擬地面效應，應用可以計算地面效應的翼型分析軟體javafoil對地效飛行器翼型的空氣特性進行分析;應用基於代理模型的優化方法對地效飛行器翼型進行優化。
  14. Finally, it got the method that how to reduce the flight accident rate and improve the safety level by the numbers. thirteen dangers during take - off was summed, after the representative take - off - accident was analysed

    在對典型的起飛事故進行分析后，總結提出了起飛所可能面臨的十三種危險，在借鑒國際飛行安全基金會提出的著陸風險意識檢查單的基礎上，研究得出起飛前機組風險意識檢查單。
  15. This paper particularly and thoroughly studied the development of air situation simulation system on a certain military information system. firstly introduce the system ' s frame and analyze the whole system by ooa technology, from which abstract some clusters and give the connection of these clusters, secondly give the arithmetic about plane ' s track, radar and sentry ' s scan function by thoroughly study the curve ' s fit and insert value method, show a better method for how to inspect plane, finally paint the system ' s flow chart. the system is basically credible by test

    本文主要討論了某軍用信息系統的空情模擬部分，首先從系統的整體功能出發，宏觀地描繪了該系統的基本框架，然後根據需求情況對該系統的各個功能運用面向對象的思想進行分析，從中抽象出多個類，設計了類與類之間的關系，並通過對各種曲線的擬合和插值演算法進行深入細致的研究，給出了求飛機飛行軌跡的演算法實現，以及雷達和哨所的方程表示，對于監測飛機的演算法結合實際給出了一種比較好的解決方法，最後繪制了整個軟體的流程圖以及描述了各個模塊的具體實現過程，完成了系統的需求。
  16. First of all, it is devoted to discuss the open - loop characteristics and the nonlinear bifurcation analysis and the maneuver ability for the super - maneuverable flight nonlinear model of the new generation fighter. then a flight control system is designed in analytical dynamical inversion method based on the time - scale separation principle

    首先，對新一代殲擊機超機動飛行的非線性模型的開環特性、分叉特性及機動能力進行分析，並以此模型為基礎，採用基於時標分離原則的動態逆控制方法設計了新一代殲擊機的飛行控制系統。
  17. Meets with component suppliers to ensure full understanding of technical issues, specifications, and application of components to fedders ' products, and their possible effects on product sound and vibration

    與供應商協調確認其對技術問題和規范的理解，從噪音和振動對飛達仕產品所產生的影響進行分析。
  18. The proposition of the data warehouse is taking development at full speed of relation data base, undertaking the parallel processing of and distributed technology as foundation, solve possession a large amount of data but useful information poor ( data rich - information poor ) comprehensive solution that information technology exist in development online analysis processing and go on technology that analyses to multidimensional data, from analyses it way obtain analysis datum of aid decision that user need from various visual angles

    數據倉庫的提出是以關系數據庫、并行處理和分散式技術的飛速發展為基礎的，是解決信息技術在發展中存在的擁有大量數據但有用信息貧乏（ datarich - informationpoor ）的綜合解決方案。聯機分析處理是對多維數據進行分析的技術，它從多視角分析途徑獲取用戶所需的輔助決策的分析數據。
  19. This article discusses the differential tail design, which will be proved to improve the roll ability for the aircraft and it will be possible for reconfiguration of the flight control processing in the design when the aircraft has a wrong

    本文就某型飛機採用差動平尾的方案進行分析，從而證明採用差動平尾操縱方式可使得飛機滾轉性能大大的提高；當飛機發生故障時，使得相應通道的控制重構成為可能。
  20. Collaborative optimization ( co ) is one of very promising multidisciplinary design optimization ( mdo ) methods. this method dissolve complex system analysis and is able to conduct the analysis of disciplines in parallel via disciplinary decompose. furthermore, the architecture of co is a natural fit to the current aircraft design organizations

    協同優化方法是多學科設計優化中比較優秀的一種方法，它消除了復雜的系統分析，使各個子系統能夠并行地進行分析和優化，而且其演算法結構與現有的飛機設計專業分工組織形式相吻合。
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