飛行成本 的英文怎麼說

中文拼音 [fēihángchéngběn]
飛行成本 英文
flying operation cost
  • 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...
  • 成 : Ⅰ動詞1 （完成; 成功） accomplish; succeed 2 （成為; 變為） become; turn into 3 （成全） help comp...
  • 本 : i 名詞1 （草木的莖或根）stem or root of plants 2 （事物的根源）foundation; origin; basis 3 （本錢...
  • 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. The grid generation of complex - shaped aerocraft is researched using the concrete object of dispenser

    本文以外形復雜的飛行器? ?布撒器為研究對象研究復雜外形的網格生成。
  3. For civil purpose. the biggest advantage of the flying air boat is that it can anything that a plane can do but at the cost roughly of one tenth, the time of staying in the air is very long ranging from 24hr. - 72hr.,

    飛艇最大的優點是凡是飛機能做的事飛艇幾乎全能做，但飛行成本比飛機便宜十幾倍，留空時間長，一般飛艇空中飛行時間可達24小時- 72小時，以上這些均是大型飛艇。
  4. In the second part, the focuses are put on the methods of realization of atc instruction speech recognition, automatic pilot reply text - to - speech, management of sky talk dialogue and aircraft state feed back display

    第二部分重點研究了本系統的管制指令語音識別、自動機長語音合成、陸空通話管理器和飛行信息反饋顯示四個模塊的具體設計方法及過程。
  5. The active vibration control aimed at aircraft empennage has huge practical values in the aspects of adding the fatigue life of vertical tail, increasing the capability and availability of the aircraft, reducing the through - life - support costs and so on

    飛行器垂直尾翼的振動主動控制對于提高尾翼的疲勞壽命、飛行器的機動性以及減小飛行器的維護成本具有較大的實際意義。
  6. Our hot balloons is driven by common fuel without any gas, as same as other normal hot balloons, it is lifted by flotage of hot air and direction controlled by gasoline motor, remote operation, safe, low risk, no ground people required leading to very low cost

    本廠生產的動力熱氣球，是用普通熱氣球燃料，不加任何氣體，和普通的熱氣球一樣，是靠熱氣的浮力上升的，汽油機控制方向和升降，遙控操作，安全，風險小，無須地面人員，飛行成本底。
  7. In order to make the terminal airspace moderated and consisted, and acquire the biggest capacity of airport, we must consider the influencing factors as many as possible, it is our final target to plan the airspace in beijing terminal unify. with the conditions that the current operation modes of parallel runway, approach and departure procedures and terminal airspace in beijing international airport, this article has analyzed the reasons of airspace congestion. this article also applies the theory of instrument flight procedure and utilizes the current facilities in beijing international airport. the design of flight procedures combining rnav procedures with instrument approach procedures may be accepted on some routes. it make the approach and departure procedure more effective, and increase the capacity of the airport more or less ; secondly, this article contrast the capacities of parallel runway in different methods under radar control, and make the conclusion that the parallel runway in dependent operation modes has the biggest capacity

    本文從目前首都機場平行跑道的運行方式、進離場程序、終端區空域的現狀入手，剖析了造成空域緊張的原因，應用儀表飛行程序設計的思想和原則，利用首都機場終端區現有的設施，某些航線可採用區域導航（ rnav ）程序與儀表進近程序相結合的飛行程序設計，優化了目前首都機場的進離場程序，在一定程度上增加了機場容量；其次，研究了雷達管制條件下平行跑道不同運行方式的容量對比，得出平行跑道獨立運行的容量最大，然後以這種這種運行方式，為首都機場設計出了平行跑道獨立運行的飛行程序；最後，分析北京終端區各機場空域對首都機場飛行程序安全、有效運行的制約因素，研究設計出了北京終端區規劃方案及規劃后的飛行程序和飛行方法，以達到增大機場的容量，適應未來航班量增加的需求。
  8. In comparison to other flying objects, it features low altitude, low flying speed, stable, safty, easy operation, low cost, specially suitable for video taking by air, geo - measuring, it is the best choice for news, moviedom, mapping ect.

    熱氣球與其他飛行器相比，其低空低速平穩安全操控簡單飛行成本低廉等特點特別適合於空中攝影攝像地形測量等的作業要求，是新聞影視測繪等行業的最佳選擇。
  9. So the aviation has installed the ground proximity warning system ( gpws ) on aircrafts since the middle of 1970s, and now is the enhance ground proximity warning system ( egpws ). this paper describes the development, components, principle and the features of the communication navigation surveillance / air traffic management ( cns / atm ), the traffic alert and collision avoidance system ( tcas ), ground proximity warning system ( gpws ), and / or the enhance ground proximity warning system ( egpws ). it particularly discuses the positive effect that ads tcas / tcas2 and gpws / egpws take on cfit and middle _ air collision. integrating with the aircrafts type. the instances and the accidents. this paper analyzes the present problems in the field of air traffic management and the new technologies resolving these problems. so that we can improve the flight safety effectively

    本文論述了新航行系統（ cns atm ） 、空中交通警戒與防撞系統（ tcas tcas2 ）以及近地警告系統（ gpws ）和增強型近地警告系統（ egpws ）的發展、組成原理及其功能特點，著重討論了自動相關監視（ ads ） 、 tcas tcas2和gpws egpws在保證飛行安全、防止空中相撞和可控飛行撞地事故中所起的積極作用，並結合具體機型和事故事例，分析了事故發生的原因和目前存在的問題，對系統提出了進一步改進的可能，以期進一步保證飛行安全。
  10. Xinda advertising airboats adopt the shape of streamline to obtain excellet ability of antiwind and reduce the flying coefficiency. operation cost of advertisers have been sufficiently considered while the design of our airboat, less gas needed, hydrogen helium inflatable. such low cost enable the advertiser recover the their expense by some flying even within one day, the colours ranging from white, yellow, colourful and can be designed according to customer s requirement

    信達飛艇在設計上充分考慮到了廣告經營者的經營成本，充氣量少，氫氦兩用。極低的運營成本可讓專業廣告飛艇的擁有者在幾個飛行起落甚至一天之內就收回一艘成品飛艇的投資。信達廣告飛艇顏色有白黃彩艇異型艇等，亦可根據客戶要求免費設計製作。
  11. Especially the quickly growing up of network economy, information technology, and finance industry challenged the traditional financial report greatly which is characteristic of historical cost principle, realized - matching principle and conservatism principle. all kinds of condemnation flew over like snowflake. it arouses us to think that whether current financial report is losing their prime value and importance gradually or not

    尤其是網路經濟、信息技術、金融業的迅猛崛起，更使以歷史成本原則、實現?配比原則和穩健原則為特徵的傳統財務報告模式受到了前所未有的挑戰，各種譴責如雪片般飛來，這不僅我們沉思；現行的財務報表是否正在逐漸失去它們原有的價值和重要性
  12. Second, by computing the trajectory of the missile and the method of analyzing cep, influences that the fighter ' s height, speed, pitch angle, the deflection angle between fighter and target, and the target moving characters make on the times of fighter attack and missile launch are deeply developed. third, by relating the motion of the missile and the fighter, the influences that fighter ' s dive angle and the deflection angle between fighter and target make on the attack field of the fighter are discussed in this paper when the fighter perform vertical and horizontal attack. criterion of attack effect is proposed focusing on attack time of the fighter, trajectory of the missile and destruction probability to the target

    本文主要完成了以下幾個方面的工作：對導彈可發射區和飛機可攻擊區進行建模，通過對導彈彈道的模擬計算，並運用典型的圓概率偏差精度分析方法，詳細討論了飛機實施攻擊時，飛機的飛行高度h 、速度v 、俯仰角、與目標的偏離角_ x及目標運動特性等對飛機攻擊時機和導彈發射時機的影響；因此，將飛機和導彈結合起來，詳細研究了飛機在垂直平面和水平平面內實施攻擊時，飛機俯沖角和與目標的偏離角_ x對飛機的攻擊范圍的影響；以飛機實施攻擊的時間t 、彈道特性和對目標的殺傷概率p來評判對地攻擊的效果；最後給出典型算例，通過對空地攻擊過程的模擬實現，對飛機飛行過載提出要求。
  13. Through calculating and analyzing basic performance, the flight characteristic of the towed system is researched. stability and control issue of carrier rocket is discussed primarily. the net result of the thesis will prove the feasibility of the scheme of towed launch

    論文通過牽引系統基本性能的計算和分析，完成牽引飛行特性的研究，同時對運載器的穩定性和控制問題進行初步的探討，最終結果將驗證牽引發射方案的可行性。
  14. The modern unmanned helicopter flight control system is generally composed of the flight control computer, the servo driving mechanism, the sensor, and the ground monitor control system etc. in this thesis the research to the helicopter flight characteristics was conducted at first, and its flight dynamic model was preliminary discussed, especially the mathematic model under hung - stop condition was formulated and the algorithm of the controller was designed in detail

    現代無人直升機飛行控制系統一般由飛行控制計算機、伺服驅動機構、傳感器、地面監測控制等分系統組成。本文首先對直升機的飛行特性進行了研究，並且對飛行動力數學模型做了初步探討，尤其對在懸停狀態下的數學模型做了較為詳盡的公式推導和控制器的演算法設計。
  15. The geometry and echoed signal models of airborne bistatic sar in general flight configuration are introduced. two - dimensional matched filtering principle is examined and theoretical relationship between resolution and bistatic sar system parameters is suggested

    本文首先分析了機載雙基地sar在任意飛行模式下的幾何模型與回波信號模型，闡述了二維匹配濾波成像機理，給出了解析度與雙基地sar系統參數間的理論關系。
  16. A chirp scaling algorithm for airborne bistatic sar is proposed, which is suitable for the flight configuration that transmitter and receiver follow parallel path with equal velocity in broadside looking mode. airborne bistatic sar echoed signal model of this particular flightpaths is derived. the model is converted into the range doppler space and is mapped from double range variables to single range variable domain

    本文建立了這種特殊飛行模式下雙基地sar的回波信號模型，推導了它在距離多普勒域的表達式，解決了信號模型從雙距離變量域向單距離變量域轉化的問題，並推導了cs因子的線性近似表達式，分析了演算法中各種近似造成的誤差。
  17. 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。
  18. As to the modelling of integrated flight / propulsion system, this paper mainly investigated and the modelling methods of flight kinetics and propulsion system thermodynamics, building up the real - time models of body kinetics. then we integrated the component - level thermodynamics model of engine, solved the problem of matching of initial points in the integrated simulation of flight / engine and the interactive parts of flight system and propulsion system

    對于綜合飛行/推進系統建模，本文主要研究的是飛行動力學和推進系統熱力學的建模方法，建立了飛機動力學實時模擬模型。並結合前人已建立的發動機部件級熱力學模型，本課題在解決了飛機/發動機綜合模擬中的起始點匹配問題的基礎上，完成飛行系統和推進系統的交互部分，最終建立飛行/發動機綜合實時模擬模型。
  19. Meanwhile it help the decision - maker to do a reasonable decision in exploiting the lines, lines arranging and the number and modal of the aircraft planned to buy as well

    同時也為航空公司進行成本決策提供服務，如開辟航線和航線布局的決策、引進飛機數量及型號的決策等。
  20. Rule # 63 : software has now taken on all the parameters of hardware ( i. e., requirement creep, high percentage of flight mission cost, need for quality control, need for validation procedures, etc. )

    軟體已經承擔了一切硬體的參數（例如，需求延伸，高比例飛行成本，質量控制需求，過程確認要求等） 。
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