飛機探察 的英文怎麼說

中文拼音 [fēitànchá]
飛機探察 英文
aicraftdetection
  • : 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...
  • : machineengine
  • : Ⅰ動詞1 (試圖發現) try to find out; explore; sound 2 (看望) call on; visit; see 3 (向前伸出)...
  • : Ⅰ動詞(仔細看; 調查) examine; observe; look into; scrutinize Ⅱ名詞(姓氏) a surname
  • 飛機 : airplane; plane; aeroplane; kite; bird; aircraft
  1. A primary surveillance radar detects and provides both range and bearing information of an aircraft within its effective coverage

    一次監雷達能測覆蓋范圍以內之距離及方向資料。
  2. Incredible this may seem, they reasoned that when the pilot checked the smoke detector during the flight, the action of pressing the detector button was a simple yet elegant way to get the time - marking process started. their suggestions were overwhelmingly accepted and results from the investigation flights in march and april this year greatly benefited from the introduction of such new practices

    這方法乍看來有點難以置信,但他們解釋當師在行途中測試煙霧測器時,師的按鈕動作可成為既簡易、又精確的時間標記。天文臺欣然接納行服務隊的建議,令今年三、四月勘行的數據處理工作簡化了不少。
  3. 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的作戰任務方式進行了航路規劃研究,包括攻擊航路和偵監視任務航路,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,對行器測概率進行定量化的研究,根據恆虛警處理技術對雷達測概率計算方法進行了總結,說明了計算單部雷達測概率問題的方法,在此基礎上對雷達網的測概率計算進行了討論,提出了相對于距離的測概率求解方法和思路,用於攻擊航路規劃中的威脅計算。
  4. Abstract : two computational techniques for inverse fight dynamics, namely derivation - iteration and integration - iteration techniques, are investigated. the application of inverse dynamics to determine control power requirements for post - stall maneuvering is researched, and a maneuvering flight trajectory based algorithm is provided, which lays a numerical foundation for simplifying design criteria for post - stall aircraft. with the model of inverse dynamics employed, a flight control mode for the outermost loop of the control system, named maneuver generator, is designed to follow desired complicated maneuvering flight trajectories. an example of rapid heading - reversal maneuver and other numerical simulations show the feasibility of the algorithm and the design idea

    文摘:考了求解輸入類行逆動力學問題的微分-迭代與積分-迭代演算法;討了利用逆動力學確定過失速動操縱效能要求問題,這構成了進一步提出過失速設計簡化判據的數值基礎;利用逆動力學設計動發生模塊進行控系統的最外環控制,以便跟蹤期望的復雜動軌跡.最速反向示例及其它數值模擬結果表明設計思想與演算法是可行的
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