flight analysis 中文意思是什麼

flight analysis 解釋
飛行分析
  • flight : n 1 飛行,飛翔;(鷹對獵物的)追趕。2 (候鳥等的)遷徙;飛行的一群。3 (光陰)飛逝。4 (思想等的...
  • analysis : n. (pl. -ses )1. 分解,分析;【數學】解析。2. 梗概,要略。3. 〈美國〉用精神分析法治療(= psychoanalysis)。
  1. The econometric analysis on the influencing factors of the capital flight from china

    中國資本外逃影響因素的計量分析
  2. Application of comprehensive two - dimensional gas chromatography time - of - flight mass spectrometry to analysis of zedoary volatile oil

    飛行時間質譜法在莪術揮發油組成分析中的應用
  3. Strength capability analysis of a flight data recorder protecting housing

    某型飛行數據記錄器防護殼體強度性能分析
  4. Three - dimensional high - density space / time soundings serve as the main body of data consisting of 3 - hr interval doppler probings, 10 - 30 min rainfall intensity, surface raindrop sizes sampling and gps - guided flight cloud physics detections with output taken at 2 - sec and 200 - m intervals. and specific systems associated therewith are developed for multiple - way communication and data collection and storage, a platform for analysis, retrieval softwares for dominant items and multi - scale cloud models - all constitute a system of techniques for meso to microscale observations and analysis. 2 ) atmospheric water resource and macroscopic rainfall properties in dry periods of spring and autumn of the target region

    以加密觀測的多普勒雷達、 3小時探空、 10 30分鐘雨強、地面雨滴譜等間隔取樣及在gps引導下的飛機雲物理探測等獲取的三維高時空密度的綜合探測為主體;配合專項設計開發的多路通訊採集存貯系統、多類信息的分析處理平臺、主要觀測項目的分析反演軟體,結合多尺度雲系模式,綜合構成層狀雲系中微尺度探測和分析處理技術方法。
  5. Effect analysis on basic flight performance for a rlss aircraft

    某機放寬縱向靜穩定度效益分析
  6. This paper introduces some ways to implement expert database systems in relational database and suggests some ways to think about expert database systems in flight record data analysis

    文中介紹了基於關聯資料庫的專家資料庫系統的實現方法,給出了在飛行記錄資料分析中應用專家資料庫系統的思路。
  7. This paper presents a wider research field - risk analysis. through the study of the effects that threat factors and error factors impact on the flight risk and adjusting performance rules, the horizontal safe corridor, threat avoidance, vertical altitude real - time modification and the fastest trajectory programming are progressed

    總結前人在該方面的研究成果,提出一個更加廣義的研究角度? ?風險分析。通過對威脅因素、誤差因素對飛行風險的作用,調整性能準則而進行了水平安全走廊設計、威脅迴避、垂直離地高度實時修正以及最快速航跡規劃。
  8. Flight simulation system plays an important role in aircraft design, performance analysis and training of pilot

    飛行模擬系統在飛行器設計、性能分析以及飛行員訓練中起著十分重要的作用。
  9. 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。
  10. According to the measuremental data of the two ammunications, the anti - designed computation and analysis of aerodynamic characteristic, flight stability, exterior ballistic characteristic for the two ammunications are studied with the advanced methods of the exterior ballistics. using the monte calo algorithm, the statistic mathematical model about ammunication ' s intensity is established and the 1000 miter vertical target intensity and the fall intensity are discussed in detail for the two ammunications. the improval potential and the main technical approachs of these ammunication ' s exterior ballistic performances are presented by compositive optimal algorithm

    根據工廠對俄ak130艦炮彈藥的測繪數據,利用先進的外彈道數值分析方法對兩種彈藥的空氣動力特性、飛行穩定性特性、外彈道特徵量等進行了反設計計算分析;採用montecarlo方法,建立了艦炮彈藥密集度性能統計分析數學模型,對兩種彈藥的立靶密集度和地面密集度進行了詳細的計算分析;利用外彈道性能綜合優化設計方法對兩種彈藥的外彈道性能指標的改進潛力和主要技術途徑進行了分析。
  11. Based on the basic principle of matrix analysis and the guiding policy for air flight route planning, and in connection with the characteristics of the domestic air service as well as their market environment, according to the article, the traditional method of matrix analysis is creatively applied to airlines ' flight route planning to provide air companies with a kind of effective, strategic analysing tool in their efforts to correctly do air route planning amid the fierce competition of the market

    摘要基於矩陣分析的原理和航線規劃的原則,結合中國航空公司的特點和市場環境,將傳統的矩陣分析方法應用於航空公司航線規劃中,為航空公司在激烈的市場競爭中進行正確的航線規劃提供了一種有效的戰略分析工具。
  12. Fourthly, we further described the process of how to analyze and design the service layer of flight information subsystem in three steps : use case model, analysis model and design model. these three steps make the whole process good traceability

    通過用例模型、分析模型、設計模型從三個不同的抽象層次和視角體現了整個分析設計過程,保證了整個過程良好的可跟蹤性。
  13. Thirdly, we discussed how to define the software architecture based on the structure and function of flight information subsystem. the software architecture defines the framework of the design and analysis process. the use of client - server architecture makes the flight information subsystem high extendibility

    在分析了飛行情報子系統的基本功能和典型用例基礎上,確定了飛行情報子系統的客戶服務器模式的軟體體系結構,從而為飛行情報子系統的詳細分析設計確定了總體框架,也保證了飛行情報子系統的可擴展性。
  14. In the condition of non - axisymmetrical stage separation in hypersonic flight, the problems of dynamics and kinematics of the validating vechicle and the launch vechicle are primarily analysised. it includes the movement of the center of mass and the rigid body of the vechicles, the relative movement of the different vechicles, the relative movement of the special parts of the different vechicles, the load analysis and the probable collision in the process of stage separation

    研究了在高超聲速狀態下非對稱級間分離過程中,驗證飛行器與運載火箭分離時的相關運動學和動力學問題。包括:飛行體質心運動和剛體運動;不同飛行體之間的相對運動;不同飛行體上特殊部位之間的相對運動;分離過程中各相關飛行體上的載荷分析和分離過程中可能發生的碰撞問題。
  15. A factor analysis of the evaluation method of safety culture in airlines flight

    航線飛行安全文化特徵評價方法的因素分析研究
  16. Analysis of panel flutter in high speed flight vehicles

    高速飛行器壁板顫振的分析模型和分析方法
  17. A analysis of flight accident

    某飛行事故分析
  18. Wake vortex separation standards are used to prevent hazardous wake vortex encounters which mainly found in the final approach course within the airport termination zone. firstly, this paper analysis the mechanism of the vortex decay and research the influence on the safety of the flight ; then. several different radar wake vortex separation standards are compared and some basic guidelines are developed to establish the future vortex standards. in addition, one kind of advance vortex classification for the civil airplane is proposed. secondly, an encounter hazard model which established for the following aircraft and a simple vortex decay model which mostly concern with the proceeding one are developed ; and a safe separation model can be derived from the both. finally, through the simulation calculation, the correctness of the vortex classification of different types of aircrafts are tested and proved

    本課題對雷達管制條件下的最小尾流間隔標準進行了較為詳細的分析和研究;首先對尾流的形成和消散機理以及尾流對飛行安全的影響做出了詳細的分析,然後就目前實行的幾種不同的最小尾流間隔標準進行了比較和分析,提出了相關的幾條準則和一種改進的機型尾流分類標準;在這之後,採用理論分析和統計數據分析相結合的方法,建立了尾流危險遭遇基本模型和尾渦消散模型;並在此基礎上對民用航空不同機型的尾流分類的合理性進行了計算和評估,為最小尾流間隔標準的確定和改進提供了初步的理論依據。
  19. 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。
  20. Information transmits instantaneously from each aircraft to large - screen displays at nsawc and records for playback for post - flight analysis of procedures and tactics

    每架飛機的相關信息實時傳送到nsawc的大屏幕顯示器上,錄制的內容將用於飛行結束后進行過程及戰術分析時的回放。
分享友人