flight balance 中文意思是什麼

flight balance 解釋
飛行平衡
  • 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...
  • balance : n 1 〈常作 a pair of balances〉 天平,秤。2 平衡,均衡,對稱;抵消;比較,對照,對比。3 (鐘表的...
  1. Article 149 in organizing and carrying out aerial work, effective measures shall be taken to ensure flight safety, protect environment and ecological balance and prevent damage to be caused to environment, residents, crops or livestock

    第一百四十九條組織實施作業飛行時,應當採取有效措施,保證飛行安全,保護環境和生態平衡,防止對環境、居民、作物或者牲畜等造成損害。
  2. When solving the tna problem based on fleet balance application, a flight pairing network model is build, by which the primary problem transferred to a directed path decomposition problem to minimize target function, and a simulated annealing algorithm is constructed

    在解決使飛機均衡使用的飛機排班問題時,本文利用航班節的網路模型將原問題轉化為一個使目標函數最小的航班節編組問題,在此基礎上構造了一個模擬退火演算法。
  3. Finally, considering the flight distance of every airline in the airline - network, using “ seat kilometre ” as the unit of the capacity, the paper optimized the capacity assignment in airline - network. as the result of above, types of aircraft and the amount of them, the flight frequency and types of aircraft were optimally constituted. the two preceding optimization procedures are all based on balance of capacity expenditure and the market share of airlines, aiming at the maximum profit in whole airline - network

    三、對整個航線網路進行運力的優化分配,首先考慮整個航線網路中具體每條航線的航程,以「座公里」作為運力單位進行,將運力在整個航線網路上優化分配,根據優化得到結果和公司擁有的機型和每種機型的數量,再對每條航線的航班頻率和機型進行優化組合。
  4. With the development of morden aero - propulsion system, the simulation technology has became one of the most important means in aeroengine design. aeroengine nonlinear mathematical models, as the basis of engine performance simulation, are not convergence favorably in entire flight scope, because of the solution limitations of nonlinear equation and the engine balance equations

    作為數值模擬的基礎與核心,目前廣泛應用的發動機非線性數學模型,由於平衡方程各種迭代解法與模型中非線性方程解法的不足,因而從根本上沒有解決模型在整個包線范圍內的收斂問題,極大地制約了發動機數值模擬技術的發展。
  5. In this thesis, ga is initially applied to aeroengine nonlinear mathematical model, the author designs ga ga act as the base of newton - raphson ( mixed algorithm 1 ) and ga alternating with newton - raphson ( mixed algorithm 2 ) three kinds of aeroengine balance equation solution methods. 8. the theoretical analysis and performance simulation results show that the aeroengine nonlinear mathematical mode not only can maintain the same efficiency with current model, but also can achieve convergence in entire flight scope when balance equation solved in mixed algorithm 2

    理論分析與模擬結果說明,採用遺傳演算法與牛頓-拉夫遜法混合的平衡方程求解方法(混合演算法二) ,既能保持牛頓-拉夫遜法的高計算效率,又具有遺傳演算法全局收斂的優點,在模型計算效率基本不變的情況下,徹底突破了常規的發動機平衡方程與模型中非線性方程解法的局限,實現了模型在整個包線范圍內的收斂。
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