track of the flight 中文意思是什麼

track of the flight 解釋
飛行航跡
  • track : vt 用纖拉船。vi 拉纖行駛。n age 拉纖。n er 拉纖的人。n 1 軌跡，輪跡，航跡，痕跡；〈pl 〉足跡。2 ...
  • of : OF ＝Old French 古法語。
  • the : 〈代表用法〉…那樣的東西，…那種東西。1 〈用單數普通名詞代表它的一類時（所謂代表的單數）〉 （a） 〈...
  • 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...
  1. Compared to the traditional technology, aviator no longer depends on the ground navigation facility but is able to flight along the precise track ; besides, airplane could land safely and accurately even under the worst visibility, which has greatly improve the safety level of flighting

    與傳統技術相比，飛行員不必依賴地面導航設施即能沿著精準定位的航跡飛行，使飛機在能見度極差的條件下安全、精確地著陸，極大提高飛行的安全水平。
  2. Its absence does not have any flight safety implication. " he said that under the maintenance and operation guidelines of the aircraft manufacturer, the aircraft could continue flying with the flap track fairing removed pending replacement

    除去整流罩對飛行安全不會構成影響。發言人指出根據飛機製造商的保養及運作指引，飛機可以在未裝上新的襟翼導軌整流罩期間繼續飛行。
  3. July 28, 2005 in response to press reports today ( july 28 ) regarding a flap track fairing falling from an a330 of ka 363 flying from tokyo to hong kong on july 22, 2005, a spokesman for the civil aviation department ( cad ) clarified that the flap track fairing did not fall off in flight as reported

    就傳媒報道有關七月二十二日，由東京返港航班編號ka363的a330型客機的襟翼導軌整流罩掉下，民航處發言人今日（七月二十八日）澄清該襟翼導軌整流罩並非如報道所言在飛行中掉下。
  4. The elements of situation maps include the information of flight track, detection range of radar, capability of weapon attack, and quantification of being attacked etc

    態勢圖元素包括飛機的軌跡信息、雷達探測范圍信息、火力攻擊范圍信息，以及受威脅程度的定量描述等。
  5. Study shows that the effect of the shock of heavy rain on an airplane in the low - level wind shear of thunderstorms is evident, the flight resistance resulted from the roughness of airplane is able to change the flight track and endanger the flight safety, whereas, the increase in the mass of airplane caused by the water film on the airframe and its wings in heavy rain is nigligible

    結果表明：雷暴低空風切變中大雨雨滴的沖擊作用是明顯的，被粗糙化的機體所產生的阻力能顯著改變飛行軌跡，並能影響飛行安全；累計在機身和機冀上的水膜厚度造成的飛機質量的增加對飛行的影響可以忽略。
  6. The detailed discussion of application of dynamic data association algorithm based on flight path dynamic prediction in this paper offers an new effective way to solving the multitarget tracking problem in track while scan radar

    通過航跡動態預測，對動態航跡數據相關在邊掃描邊跟蹤雷達的數據處理方面應用做了詳細討論，為解決邊掃描邊跟蹤雷達的多目標跟蹤問題給出了一種有效的新途徑。
  7. Early warning system of missiles is an real - time infrared reconnaissance camera based on satellite platform, it can simutaneously reconnoiter, discriminate and track the enemy missile, then obtain the information about the missile ’ s flight parameter

    本文研究的導彈預警系統是基於衛星平臺的紅外實時傳輸偵察相機設備，它可以實時偵察、辨別、跟蹤敵方飛行導彈，在短時間內獲取導彈飛行資料。
  8. The algorithm of strapdown inertial navigation system is also discussed and then use the flight - track generator to give a simulation, since a closed loop feedback integrated navigation system is designed in this paper, and the output of the filter must feed back to the strapdown inertial navigation system, the analysis of the algorithm in strapdown inertial navigation system is important. the scheme to design the trajectory of gps and the simulation of gps constellation are then studied, the simulation of gps constellation is given from the calculation of vernal equinox base on the principle of celestial mechanics, this method of different from other methods given by other paper and is useful to the research of satellite navigation system. a new method to abstract noise modal in integrated navigation system is proved to be useful in practice, this method, which is given by use the principles of stochastic processes, statistics, time series analysis, and system identification, is suitable for the kalman filter in integrated navigation system

    如航跡產生器的設計，該航跡產生器是研究組合導航問題的前提，從國外一些研究組合導航系統的文獻中可以看出，設計這樣一個航跡產生器是非常必要的，所以本文自行設計了這樣一個系統；還討論了捷聯慣性導航系統中捷聯解算的方法，並進行了模擬研究，由於在本文設計的閉環反饋式組合導航系統中，對捷聯慣導系統的平臺誤差進行閉環控制，需要將濾波器輸出的校正量反饋到捷聯解算內部，所以必須對捷聯解算進行深入的研究和分析，更何況捷聯解算問題本身也是導航界的一個熱門研究課題；另外，本文還介紹了gps軌道及其星座模擬的設計思想和方案，與以往gps軌道和星座模擬不同的是本文從天體力學中計算春分點開始，逐步進行gps軌道及其星座模擬，這樣的設計方法對從事衛星導航的研究工作是有價值的；還對組合導航中誤差建模方法進行了研究，綜合運用隨機過程、概率統計、時序分析及系統辯識等方面的理論提出了一套適合組合導航卡爾曼濾波的誤差建模方法，並運用實際研究工作中的測量數據對該方法進行了驗證。
  9. Implementation of an interface agent in the field of emulator of space - flight track

    開發程式控制交換機多媒體模擬訓練系統的支撐軟體環境
  10. The uav can fly along the scheduled fight path with correct attitude by the research of the control law of portrait flight track and transverse coordinated turn

    文中通過研究無人機縱向航跡跟蹤和橫側向協調轉彎的控制律使得無人機可以以下確的姿態沿預定的航跡飛行。
  11. There are many factors that may affect the aircraft s flown track - the wind speed and direction relative to the aircraft s intended flight path, the performance characteristics of the aircraft, tolerances in navigational aids and different piloting skills and techniques etc. in practice, the flown tracks may deviate either side of the nominal centre line shown in the map in

    飛行中的飛機不能如火車般緊貼路軌行走。飛機在飛行中會受多方因素影響：這包括相對于飛行航道的風速及風向、飛機的操作性能、導航儀器的偏差、機師駕駛技巧等。基於以上原因，實際的飛行航道可能有別于
  12. A noise and flight track monitoring system has been installed to assist the department to monitor the implementation of the noise abatement programme

    民航處已安裝了一套飛機噪音及航跡監察系統，監察減低飛機噪音計劃的實施情況。
  13. An aircraft noise and flight track monitoring system was installed in june to help evaluate the track keeping performance and noise impact of flights operating to and from the kai tak airport

    民航處於六月安裝了一套航機噪音及航道監察系統，以便評估航機按航道飛行的表現及在啟德機場升降時所造成的噪音。
  14. At the end of the dissertation, the fuzzy pd track tail controller is designed. the pd controller and controller of attitude angle are made up of flight control system of helicopter

    最後，本文設計了直升機模糊pd軌跡跟蹤控制器，與姿態角控制器相結合，完成了對整個飛行控制系統的設計。
  15. 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。
  16. Pilots are required to follow these routes unless instructed otherwise by atc. for the efficient management of limited airspace, atc may give pilots a more direct route to their destination or a radar heading for separation with other traffic. 8. it should be noted that an aircraft in flight cannot follow a track precisely like a train running along a railway track

    為有效地利用有限的空域，航空交通管制員不時需要指示機師使用更直接往目的地的航道，或在交通繁忙時，航空交通管制員會指示機師採用其他方向以保持航機間之適當距離。
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