殲擊機 的英文怎麼說

中文拼音 [jiānjījī]
殲擊機 英文
fighter plane; fighter
  1. Air crew must love, love - made fighter ; friendship first, competition second

    隊員必須熱愛空戰、熱愛國產殲擊機；友誼第一，比賽第二。
  2. The fighter planes quickly disengaged ( from the combat )

    殲擊機很快（從戰斗中）撤出了
  3. He graduated with excellent grades in 1987, and became a pilot in the air force, fulfilling a long cherished dream. he flew various types of fighter aircraft and rose to squadron leader. with 1, 350 flight hours, he achieved a high technical competence ; he was ranked a pilot of the first class and was twice awarded third - class merit, in 1992 and 1994

    在職期間，曾任中隊長、領航主任，駕駛殲擊機、強擊機等機型，並曾安全飛行一千三百五十小時，技術高超，獲評為一級飛行員，一九九二年及九四年，先後兩次榮立三等功。
  4. This actuator is used in the longitudinal control system of fighter t improve longitudinal control and stability, and is a power actuating unit of autopilot

    用於殲擊機縱向操縱系統，改善縱向操穩性能，也是自動駕駛儀的輸出執行部件。
  5. It has solved the problem of weak robust when the linear control theory is used to control a complicated nonlinear systems like airplane

    克服了單純用線性控制系統理論來控制象殲擊機這樣的復雜非線性系統魯棒性能較差的問題。
  6. We can see fighters soaring in the sky

    我們能看到殲擊機在天空中翱翔。
  7. Air combat is the basic task of the fighters

    空戰是殲擊機的基本任務。
  8. A fourth generation stealth fighter jet would help, too

    一臺第四代秘密行動噴氣式殲擊機即將問世。
  9. Fourthly, a discussion is devoted to study the integrated flight / propulsion control system

    接著，對新一代殲擊機的綜合飛行/推進控制系統進行研究。
  10. Firstly, many examples, simulating the steady and unsteady viscous flows around several wings and some aircraft, are given in this paper

    以多種機翼和某殲擊機為算例，分別對其定常及非定常粘性繞流進行了數值模擬。
  11. Made any fighters assault group members are not allowed to cheat in any form, any person who was found cheating. will be expelled from the team

    任何國產殲擊機戰隊隊員以任何形式的作弊都是不允許的，任何人被發現作弊，將驅逐出隊。
  12. All team members must unite with domestic assault group of fighters center, or not make any detrimental impact on the reputation of the assault group

    隊員必須一切以國產殲擊機戰隊團結為中心，不得作出任何影響或有損戰隊聲譽的行為
  13. On the basis of designing robust flight control system of the new generation fighter, this dissertation is devoted to the design of the integrated fire / flight control system and the integrated flight / propulsion control system and the integrated fire / flight / propulsion control system

    以研究新一代殲擊機的魯棒飛行控制系統為前提，進一步研究其綜合火力飛行控制系統、綜合飛行推進控制系統以及綜合火力飛行推進控制系統的魯棒控制問題。
  14. Aim to plan optimal routes for a type of cruise missiles ( cms ) which can avoid the firepower units as surface - to - air missiles, antiaircraft guns, fighter planes, electromagnetism impulse and terrain obstacles and have the shortest length as well as consume the least oil

    摘要目的設計優化一類巡航導彈航跡，且航跡滿足避開地空導彈、高炮、殲擊機群、電磁脈沖等火力單元和地形地物障礙，並且滿足航跡路徑長度短、耗油量少等約束條件。
  15. It is one of the most common illusions in flight among the pilots of fighter planes. american researchers investigated 105 pilots of fighter planes, according to the survey, 50 per cent pilots had experienced ci in flight. our survey in 1999 is analogous to theirs

    據美國1998年進行的一項105名飛行員的調查顯示：有50的飛行員在飛行中體驗過這種錯覺，我們在1999年調查了91名我軍殲擊機飛行員，也發現有42的飛行員在以往飛行中產生過科里奧利錯覺。
  16. Then, because of the characteristic of complex engineering systems like fighters, such as modeling difficulty, multiplicity work situations, difficulty and expensiveness for test, a new kind of fast fault predictor is designed based on an improved k - nearest neighbor method, which neither need math model of system nor need data for train and knowledge

    其次，針對殲擊機等復雜工程系統建模困難、工作情況多樣、試驗困難且代價高昂的特點，提出了一種改進k近鄰密度估計方法，設計了一種完全既不需要系統數學模型也不需要故障訓練數據和先驗知識的實時故障預報器。
  17. First of all, it is devoted to discuss the open - loop characteristics and the nonlinear bifurcation analysis and the maneuver ability for the super - maneuverable flight nonlinear model of the new generation fighter. then a flight control system is designed in analytical dynamical inversion method based on the time - scale separation principle

    首先，對新一代殲擊機超機動飛行的非線性模型的開環特性、分叉特性及機動能力進行分析，並以此模型為基礎，採用基於時標分離原則的動態逆控制方法設計了新一代殲擊機的飛行控制系統。
  18. The control scheme is successfully applied to the simulation of fighter control system. the simulation results demonstrate that the control scheme is effective

    控制方案成功的應用於殲擊機飛行控制系統中，模擬結果表明了方法的有效性。
  19. Utilizing the force identification approaches above mentioned, experiments on the model of a supersonic fighter and on a wheel - rail coupled system are performed respectively, in order to verify the validity of the proposed theories in this dissertation

    利用上述動載荷識別模型，本文分別對超音速殲擊機模型和高速鐵路輪軌耦合系統作了動載荷識別實驗驗證。結果表明，本文提出的方法能有效地進行未知激勵下的動態載荷識別及作用位置識別，從而驗證了本文理論的有效性。
  20. Second, the t - s fuzzy model is adopted for modeling of the known nonlinear system approximately, meanwhile fuzzy - model - based h tracking control law is designed to track the desired output signal

    其次，利用t - s模糊模型對系統進行近似建模，應用基於模糊模型的模糊h _跟蹤控制律對殲擊機進行輸出跟蹤控制。
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