計器飛行方式 的英文怎麼說

中文拼音 [jìqìfēihángfāngshì]
計器飛行方式 英文
ifr instrument flight rules
  • 計 : Ⅰ動詞1 （計算） count; compute; calculate; number 2 （設想; 打算） plan; plot Ⅱ名詞1 （測量或計算...
  • 器 : 名詞1. （器具） implement; utensil; ware 2. （器官） organ 3. （度量; 才能） capacity; talent 4. （姓氏） a surname
  • 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...
  • 方 : Ⅰ名詞1 （方形; 方體） square 2 [數學] （乘方） involution; power 3 （方向） direction 4 （方面） ...
  • 式 : 名詞1 （樣式） type; style 2 （格式） pattern; form 3 （儀式; 典禮） ceremony; ritual 4 （自然科...
  • 飛行 : flight; flying; aviate; voyage; volitate; hop
  • 方式 : way; fashion; pattern
  1. Ifr instrument flight rules

    計器飛行方式
  2. This dichotomy misses the fact that ai has quietly been lending its more modest achievements to real - world computing for quite some time. every other movie and sci - fi tv series features the omnipotent space ship computer with the personable talking head ; in the real world, computer programs with connections to sensors and tools, using very mundane input and output, make many tasks in space possible that would be beyond the accuracy and processing power of humans

    一半以上的科幻電影和科幻電視連續劇裏面都有一臺無所不知的宇宙飛船電腦，它擁有一個談吐文雅的腦袋；在現實世界里，電腦的計算機程序總是和很多的傳感器以及各種工具連在一起，使用一些非常普通的方式進行輸入輸出，盡可能快速及時地完成很多任務，這些任務對人類來說是過于精確和難以控制好的。
  3. Secondly, towed system is considered as many rigid body systems. according to research approaches of many rigid body systematic dynamics, the towed systematic engagement calculating models is derived ; according to actual course of the towed flight, deriving mathematics model of the course of taking off and towed flight of the towing plane and of carrier rocket, and corresponding parameter calculate models

    其次將牽引系統作為多剛體系統宋考慮，根據多剛體系統動力學研究方法，建立牽引系統約束方程，由此推導出約束力計算公式；根據牽引飛行實際過程，推導出載機、運載器在起飛階段，巡航飛行階段的數學模型，以及相應的參數計算模型。
  4. With c + + language, iods is composed of traditional optimization methods, knowledge base, inference machine, knowledge acquisition and graphic user interface ( gui ) in windows 2000. this integrated synthesis system performs the intelligentized optimization design for asrv, including the following items : production deduction strategy, knowledge handling technology, traditional optimization methods, evolutionary algorithms and the object - oriented strategy

    此系統利用c + +語言在windows2000環境下編制而成，由優化演算法庫、知識庫、推理機制、知識錄入和圖形用戶界面等幾部分構成；該系統將產生式推理技術、知識處理技術、基於數學規劃的優化演算法、現代優化演算法以及面向對象程序設計方法綜合成一個有機的整體，形成了一個針對再入飛行器氣動布局優化設計的智能優化設計平臺。
  5. It can construct a reference path with lowest danger for the uav ( unmanned aerial vehicle ) by accounting for some aircraft performance characteristics, the mission goals, the threat information and the terrain information. this paper puts emphasis on the study of path planning algorithms and the analysis of uav missions. the main contributions are summarized as follows : ( 1 ) the threat environment, mainly as the radar threat, is studied and the detection probability of the aircraft is analyzed

    本論文主要根據無人機的作戰任務方式進行了航路規劃研究，包括攻擊航路和偵察監視任務航路，具體內容包括以下幾個方面： （ 1 ）本論文分析了威脅空間的威脅計算問題，對飛行器探測概率進行定量化的研究，根據恆虛警處理技術對雷達探測概率計算方法進行了總結，說明了計算單部雷達探測概率問題的方法，在此基礎上對雷達網的探測概率計算進行了討論，提出了相對于距離的探測概率求解方法和思路，用於攻擊航路規劃中的威脅計算。
  6. Secondly, the stability of designed afcs is analyzed and an amalgamation control mode of damper and stability augmentation control system is put forward in the paper

    其次，文中對設計的飛控系統進行了穩定性分析，提出阻尼器與增穩控制系統相融合的控制方式。
  7. Dfse, which is an integrated system implemented by utilizing the distributed simulation technologies, will be widely used to meet the need of flight simulation in the demonstration, design or experiment aspect of an aerospace vehicle and other

    本文研製的dfse系統是根據飛行器系統細粒度模擬的具體需要來設計完成的一套比較完整的分散式飛行模擬通用平臺，它在飛行器系統論證、設計與模擬實驗等方面以及相關領域中都有著廣闊的應用前景。
  8. Unlike traditional differential geometrical method, the robust adaptive neural net - based control emphasizes on the theory and application of intelligence control in nonlinear system that is weighed by robust performance index. the problem of robust reliability and stability in a kind of weak nonlinear system is first proposed in the dissertation, and then it deeply analyses and discusses the problem of how to design track controller in strong nonlinear system with uncertainties and external disturbance on the premise of guaranteeing the whole system ' s robust performance index. the distributed 3d flight simulation platform is mainly used to validate real - time program and evaluate the efficiency of advanced flight control laws, therefore, some theories and techniques related to the platform are also introduced

    基於神經網路的魯棒自適應控制研究和分散式三維飛行模擬平臺的構建是本論文研究的兩個主要內容，與傳統微分幾何方法不同的是，基於神經網路的魯棒自適應控制側重於智能控制方法在以魯棒性為性能指標的非線性系統中的理論和應用研究，論文以一類弱非線性系統的魯棒可靠鎮定問題為引線，逐步深入地分析和探討了在保證整個被控系統魯棒性能指標的前提下，對于幾類具有不確定性和外部擾動的強非線性系統跟蹤控制器的設計問題；分散式三維飛行模擬平臺主要用於先進飛行控制律的實時程序驗證和效能評估之用，因此關于平臺的一些開發原理和技術方法也在文中給出了介紹。
  9. According to the models mentioned above, this paper lays emphasis on accounting the method of analyzing and designing the cruise aircraft ' s control system adopting the classical control theory, and then calculates the parameters of it

    根據以上建立的模型，本文重點論述了採用經典控制理論分析此巡航式飛行器控制系統的方法，並計算出此巡航式飛行器飛行控制系統的參數。
  10. In the end, the aircraft ' s optimized control system designing methods and the approaches of developing simulation software of this aircraft ' s control system based upon matlab are also briefly discussed

    最後，本文還對此飛行器控制系統的最優控制設計以及基於mtalab的巡航式飛行器控制系統模擬軟體設計方法進行了簡單的探討。
  11. It can be seen that the structure and parameters of the flight control system are reasonable ; the performance can meet the need of the task

    通過給出的部分模擬結果可以看出，本文得出的巡航式飛行器飛行控制系統結構合理，設計方法可靠，系統參數可以滿足該飛行器控制的總體性能要求。
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