飛行排程 的英文怎麼說
中文拼音 [fēihángbèichéng]
飛行排程
英文
flight scheduling- 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...
- 排 : 排構詞成分。
- 程 : 名詞1 (規章; 法式) rule; regulation 2 (進度; 程序) order; procedure 3 (路途; 一段路) journe...
- 飛行 : flight; flying; aviate; voyage; volitate; hop
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Furthermore, 100 members who performed exceptionally well are invited to join one of the overseas trips to boeing in seattle, u. s., airbus in toulouse, france, or and bae flying school in adelaide, australia. please visit the
此外,一百名優秀的會員獲安排於2004年8月參加一項海外旅程,分別前往美國西雅圖的波音公司及法國圖魯茲的空中巴士飛機製造廠或位於澳洲阿德萊德的飛行學院。Board your overnight transatlantic flight to france
行程安排妥當,不緊促,不鬆弛,長途搭乘飛機。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。The cad has maintained close liaison with the civil aviation authorities of the mainland and macau in relation to the development of flight procedures and atc co - ordination arrangements
香港民航處與內地及澳門的民航管理部門在發展飛行程序及航空交通協調的安排上一直保持緊密的聯系。Firstly, a 0 - 1 integer programming mathematical model is constructed to describe tail - number - assigning work happened in domestic airline, since the problem is npc, a unified polynomial algorithm which satisfies engineering requirement is unavailable. illuminated by the practical experience, a specific tna problem is classified into one of three typical tna modes : tna based on fleet dispatching commands, tna based on fleet balance application, tna based on minimum fleet requirement ; secondly, by simplifying and relaxing some minor constraints, corresponding mathematical models and heuristic algorithms are reconstructed for each typical tna mode ; finally, computing complexities are discussed
為此論文在借鑒手工編制排班計劃經驗的基礎上,將一個具體的飛機排班問題,歸結為三種典型排班模式中的一種,即:基於飛機調度指令要求的排班問題,基於飛機使用均衡要求的排班問題和基於最少需用飛機數的排班問題,對于每種典型的飛機排班模式,在對次要的約束條件進行簡化、松馳的基礎上構造出相應的能夠滿足工程應用要求的啟發式演算法,並分析了演算法的復雜性。Easy schedule with all the high - lights and least time spend on the road
行程安排妥當,不緊促,不鬆弛,長途搭乘飛機。" unlike the conventional approach procedures, aircraft on cda will be arranged to approach from a higher altitude and descend continuously to join the final approach flight path for the runway being used
該處發言人說:持續降落模式與傳統進場程序不同,採用新模式的航機會安排在較高的飛行高度進場,然後持續下降至航道之最後進場階段。Abstract : in this paper, a new method for dynamic measurement of engineexhaust using tofms ( time - of - flight mass spectrometer ) is presented, and a high - speed data acquisition system is designed
文摘:本文介紹了利用飛行時間質譜儀( tofms )對發動機發動過程中的排氣成分進行動態檢測的方法以及為此開發的高速數據採集系統。3. wth application of large - scale computational software anasys - dyna, the case of elastic impact to each other of two recta - ngular cross - section rods has been implemented and also compared with theoretical results, which maks good agreement and draws very helpful practical experiences to use some techncal parameters in the program. eventually, the a real - world aircraft windshield shell structure impacted by a flying bird has been simulated through fem numerical computation, and meanime, an engineering predical experimeni of bird sttiking to the windshield in some type of aircraft has been performed
3 、應用大型科學計算程序anasys - dyna ,對彈性體碰撞進行了數值計算驗證並與理論結果對比,獲得了計算參數應用的實踐經驗;在此基礎上,進行了鳥體撞擊飛機風擋結構動力學響應的實際數值計算,與此同時安排了工程鳥體撞擊試驗,並就兩者計算結果給予了細致分析對比,獲得了良好的一致性結論。Different from other algorithms, the algorithm in this paper that adopts sliding sequencing window does not search all sequences generated by whole aircraft queue, but search possible sequences generated by some aircraft for certain positions fixing in optimized queue. so, this algorithm can break through the bottleneck of computation penalties caused by the use of cp algorithm and make it easy to reschedule the queue of more than 10 aircraft in heavy traffic
與其它演算法不同,本文提出的排序演算法引入了滑動排序窗的概念,它不用對隊列中全部飛機的所有排序可能進行搜索,而只需對那些與最終排序結果中的某些特定位置相關的飛機(當前窗)所產生的排序可能進行搜索,依次移動窗體就可完成對所有飛機的排序過程。Referring to the newest proposal on aircraft maintenance of the military of u. s. a and aimming at the problems of the information management system of traditional civil aviation maintainence engineering, this thesis came up with a new system - digital integrated maintenance and support information system ( dimsis ), which is made up by the technologies of computer network, database, communication engineering, software engineering and etc. after its building, most of the requirements of the domestic airlines on information technologies will be met
該系統將計算機網路、數據庫、通信工程、軟體工程等技術有機結合,首先用internet intranet技術構建企業局域網,然後將飛機維修最原始的資料? ?維修手冊電子化錄入到主機系統,達到在各終端的快速信息訪問,並針對停機坪維修的特點,將有線網進行延伸,在機場搭建基於無線局域網技術的便攜式飛機維護助手pma ,提高飛機的故障排除速度與派遣放行率。分享友人