飛行軌跡 的英文怎麼說

中文拼音 [fēihángguǐjī]
飛行軌跡 英文
flight path
  • 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...
  • 軌 : Ⅰ名詞1. （路軌;軌道） rail; track 2. （比喻辦法、規矩、秩序等） rut; path; course Ⅱ動詞[書面語] （遵循; 依循） follow
  • 跡 : 名詞1 （留下的印子; 痕跡） mark; trace 2 （前人遺留的建築或器物等） remains; ruins; vestige 3 （...
  • 飛行 : flight; flying; aviate; voyage; volitate; hop
  • 軌跡 : 1 [數學] （某點在空間移動的路線） locus; trajectory; trail; travel; path; way; [電子學] trace; li...
  1. The guidance scheme includes a trajectory planner that generates a feasible flight trajectory and a control law that achieves bounded tracking of the downrange and crossrange distances as functions of energy

    其中，軌跡規劃器可產生一個可行的飛行軌跡。控制律作為能量的函數可實現再入段對縱向和橫向航程的有界跟蹤。
  2. The flight path would then either intersect the earth, or go off into space.

    飛行軌跡不是和地球相交，就是離開地球而進入宇宙空間。
  3. Methods for intelligent tactical flight path planning

    智能化戰術飛行軌跡規劃方法研究
  4. Starting from straight and level flight after the helicopter passes the pilot, the helicopter is smoothly pulled through a loop ( aft cyclic )

    先保持水平直線飛行，當直升機通過操控者后，開始平滑地拉高機頭（打升舵） ，使飛行軌跡成為一個環狀。
  5. Because the main problem in weapons delivery is getting your flight path ( ground track ) to intersect the target

    因為空投武器的主要問題就是如何讓你的飛行軌跡正好從目標上空掠過。
  6. Even if a projectile can adjust its flight path, it still must contend with the prospect of enemy electronic jamming

    即使要一發炮彈能夠調整其飛行軌跡，還是必須考慮敵方電子干擾的情況。
  7. Direct side force control ( dsfc ) comes into being with the appearance of act ( active control technology ). through maneuvering the vertical canard to produce side force, people can control a aircraft easily. so the trajectory of a vehicle can be controlled precisely, and it ' s maneuverability is greatly improved

    直接側力控制是隨著主動控制的提出而出現的，採用直接側力控制，可在不改變飛機姿態的條件下，直接通過控制面造成側力來操縱飛機機動，從而達到精確控制飛行軌跡和增強機動能力的目的。
  8. 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。
  9. Iliff, k. w., “ parameter estimation for flight vehicles, ” journal of guidance, control, and dynamics, vol. 12, no. 5, 1989, pp. 609 - 622

    詹銘堯， 「非線性飛行動力系統參數識別與飛行軌跡重建， 」國立成功大學航空太空工程研究所碩士論文， 1997年
  10. The system was developed by setting the function pages, achieving the management of the data transmission and integrating the geographic information system ( gis ) into system to achieve the planar display of the flying track

    系統建立各個功能頁面，實現分佈模擬系統內部的實時數據通訊管理，集成地理信息系統實現飛行軌跡二維態勢顯示。
  11. In ccs ' c3x - ' c4x compile environment, using composite programming method of c and assemble language, the author debugs each port of the hardware circuit system, analyses interrupts mechanism and bootloader mechanism of the dsp, develops the system of generating flight orbit data

    其次，在ccs ' c3x - ' c4x編譯環境下，採用c語言和匯編語言混合編程的方式，初調了硬體電路系統的各個埠，分析了dsp晶元的中斷和bootloader機制，開發了飛行軌跡數據生成系統。
  12. Based on this main idea, first the thesis discusses the mathematics model of gyro and accelemeter, the initial alignment of north - pointed strapdown inertial navigation system, the method of calculation navigation, the method of generating flight orbit data, the method of ins / gps integrated navigation in detail. then the thesis develops the system generating flight orbit data and the system of real - time simulating strapdown inertial navigation with vc + + 6. 0

    論文以此為核心展開：首先詳細討論了陀螺和加速度計的數學模型、指北式捷聯慣性導航系統初始對準和導航解算的演算法、飛行軌跡數據生成演算法、 ins gps組合導航演算法；然後利用visualc + + 6 . 0開發出飛行軌跡數據生成系統、捷聯慣性導航實時模擬系統。
  13. Trajectory tracking was completed through the outer loop

    飛行軌跡的跟蹤則通過外迴路來實現。
  14. Abstract : a method named multi - times optimization is presented to solve the multi - specification optimization problem, which is difficult to solve using the variational optimal theory. in the method several demands are reduced to some sub - tasks. in every subtask a demand that can not be transformed into bound condition is taken as performance specification for optimazation, and the other demands are taken as bound conditions. by means of the method, the arrival time, number of turn, turn angle of the aircraft in the terminal area are selected as performance specification separately, and the general character of optimal flight route in the terminal area is given

    文摘:為了給飛機提供一條能滿足多種指標要求的最優飛行軌跡，針對變分最優理論難以求解多指標優化問題，提出了命名為多次優化的方法，即將多要求的優化任務分成先後相繼的多次任務，每次任務中選取一種不能邊界轉化的要求作為最優性能指標，而其餘要求轉化為邊界條件.利用這一方法以時間、轉彎次數、轉彎角度為最優性能指標給出了終端區最優飛行軌跡的一般特徵
  15. You can keep your eye on the ball all you want, but if your judgment is poor you will see the ball with perfect clarity as it travels right on past your racket and hits the back fence ! !

    你可以盯住所有的球，但是如果判斷力不足，縱然很清晰地看到了球的飛行軌跡，也打不著它，任由網球擊中后網！ ！ ！
  16. The problem is then fed to a nonlinear programming routine to solve for all parameters. the flight dynamics model with yawing motion of uh - 60a is given, scale factors of state variables and control variables are applied based on the consideration of algorithm convergence. then, the optimization of trajectories is expressed as optimal control problem with a performance index constrained by helicopter performance limits, faa regulation and so on

    首先，建立帶偏航運動的直升機點質量模型，然後對狀態變量和控制變量進行無量綱處理，因為狀態變量和控制變量量值相差較大，這使得優化演算法收斂效果變差，所以需要選擇適當的縮放因子，最後把直升機單臺發動機停車后的飛行軌跡表示成一個最優控制問題，即在考慮直升機性能限制和far規范后，指定一個優化性能指標，選擇合適的路徑約束，然後再解最優控制問題。
  17. The actual - operating parameter ( level angle, pitching angle, speed etc ) of theodolite are measured by code check of theodolite, and sent to computer by the interface

    教練員可通過系統提供的輸入界面輸入目標的位置參數及目標飛行軌跡的特徵點。經緯儀的實際運動參數由經緯儀自身的碼盤測出，並通過計算機介面輸入到計算機中。
  18. Implementing the 3 - d visual system of air combat simulation with the help of the computer by using new technologies, such as opengl, visual c + + and oop. the procedures of fighting can be displayed intuitively. at the same time, the flight tracks of simulation can be recorded and analyzed, which helps to analyze and evaluate the performances of the current fighters in service qualitatively and quantitatively

    3 、運用opengl 、 visualc + +與面向對象編程等技術，實現了基於pc機的飛機模擬空戰三維可視化系統，可以比較直觀地顯示戰斗機的空戰過程，同時也可記錄分析模擬飛行軌跡，從而對現役戰斗機的性能進行定性和定量的分析評估。
  19. Abstract : this paper presents an inverse simulation algorithm of determining the pilot control law as well as the time histories of helicopter velocity, angular velocity and flight altitudes to follow a given helicopter maneuver flight path

    文摘:本文給出了一種直升機機動飛行的逆模擬方法以計算跟隨預定飛行軌跡的駕駛員操縱。
  20. Based on gyro - free inertial navigation theory while revolve about mems accelerometer and dsp, this dissertation mainly focuses on the research of gyro - free inertial measurement unit for shell flight path measurement - the first step for guidance

    本文以無陀螺慣性導航理論為基礎，以微機械加速度傳感器、高性能dsp處理器為核心，研製應用於某型炮彈的無陀螺慣性測量系統，該系統將用於炮彈飛行軌跡的測量，是實現炮彈制導的第一步。
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