駕駛儀 的英文怎麼說

中文拼音 [jiàshǐ]
駕駛儀 英文
driverscope
  • : Ⅰ動詞1 (使牲口拉車或農具) harness; draw (a cart etc ) 2 (駕駛) drive (a vehicle);pilot (...
  • : 動詞1. (飛快地跑) (of a vehicle, etc. ) speed 2. (開動) sail; drive
  • : 名詞1 (人的外表) appearance; bearing 2 (禮節; 儀式) ceremony; rite 3 (禮物)present; gift 4 ...
  • 駕駛 : drive; pilot; steer; aviate; helm; driving
  1. Meanwhile, it is also useful for automatic pilot design

    同時,該方法對自動駕駛儀的設計也有一定的參考價值。
  2. Design of breakdown diagnose fuzzy - expert system for shore - to - ship missile automatic pilot

    岸艦導彈自動駕駛儀故障診斷模糊專家系統設計
  3. Steering by automatic pilot and by magnetic compass in stead of automatic pilot, measure the exactness of magnetic compass by qualified calibrator and provide compass adjustment card

    自動駕駛儀操舵和用磁羅經代替自動駕駛儀,通過合格的校準器來測定羅經的正確功能並提供羅經校正卡。
  4. Firstly, the random mathematics model of the guidance system is set up, with the random factors such as the seeker, the guidance law, the automatic pilot, the dynamics, the relative kinematics taken into account

    首先進行反輻射無人機系統的隨機建模,包括導引頭、制導律、自動駕駛儀,機體動力學,相對運動學等,建模時必須考慮隨機因素的影響。
  5. Identical autopilots are used to control the pitch and yaw motions if the missile has two planes of symmetry.

    如果導彈有兩個對稱面,則使用相同的自動駕駛儀控制俯仰和偏航運動。
  6. In order to design the autopilot for a rear controlled missile we must make a first estimate of the required aerodynamic derivatives.

    為了設計尾部控制導彈的自動駕駛儀,我們必須首先估算一下所需要的氣動力導數。
  7. Verification regulation of autopilot system test bench " - 3

    - 3型自動駕駛儀校驗
  8. 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。
  9. Verification regulation for command pilot instrument test bench b - 4

    B - 4指令駕駛儀測試臺試行檢定規程
  10. This design method overcomes the traditional autopilot ' s disadvantage that should shift the autopilot ' s gain according to flight phase ; it also can make the btt missile fly stably along the whole trajectory, and can intercept a maneuvering target accurately

    該設計方法克服了傳統自動駕駛儀在控制導彈飛行中需逐段切換增益的不足,能控制btt導彈在大空域內沿全彈道穩定飛行,並能精確攔截機動目標。
  11. Considering that the state variables can be measured easily and the autopilot can be designed expediently, the btt missile ' s control model in which all trajectory states can be measured is presented in this thesis

    並考慮到狀態變量的可測量性和自動駕駛儀設計的方便性,建立了全彈道可測量的btt導彈控制數學模型。
  12. Autopilot tends to drop a wing when fuel imbalance reaches 500 pounds

    當燃油不平衡達到500磅時,自動駕駛儀試圖沉下一側機翼。
  13. The aircraft engines, autopilot, and navigation system are absolutely reliable.

    飛機發動機,自動駕駛儀和導航系統絕對可靠。
  14. Cockpit installation. standard pilot. minimum useful dimensions

    艙設備.標準駕駛儀.最小有效尺寸
  15. Cockpit installation. standard pilot. maximum useful dimensions

    艙設備.標準駕駛儀.最大有效尺寸
  16. To avoid high frequency oscillation in the course of autopilot design, damping coefficient value was treated as a constraint, the rise time was taken as objective, and the other performance criteria were taken as constraints, then the robustness design problem was solved by multi - objective optimization method

    摘要在導彈控制系統設計過程中,考慮了自動駕駛儀的高頻振蕩問題,將其轉化為系統的一個約束條件,同時把上升時間轉化為目標函數,其他設計指標視為約束條件,採用有約束多目標優化的方法解決了系統魯棒性設計問題。
  17. And the traditional designed autopilot has poor robustness, so it should shift the autopilot ' s gain for the btt missile flying stably along the whole trajectory

    又由於用傳統方法設計的自動駕駛儀魯棒性不高,為控制導彈沿全彈道飛行,需逐段切換自動駕駛儀的增益。
  18. Consequently, computational models of all subsystems are constructed, such as the strapdown inertial navigation system ( sins ), the control loop applied in self - control period, the guidance system by applying the technology of television ( tv ) guidance and the guidance law of proportion navigation, the autopilot by applying the technology of overload control in terminal control period, and so on

    建立導彈各個子系統的計算模型,主要有捷聯慣性導航系統、彈體、導彈自控段的控制穩定迴路、採用電視制導和比例導引制導律的導引系統,以及採用過載控制的自動駕駛儀,然後在此基礎上建立導彈各系統模擬模型。
  19. The main task of this dissertation is to digitize an autopilot system installed in a certain lateral airliner. the difficulty of this task is to design and manufacture a dissimilar redundancy fault - tolerant autopilot computer

    本論文的主要工作是對某支線客機自動駕駛儀進行數字化。該項工作的難點是非相似余度容錯飛控計算機的研製。
  20. By adopting the full state feedback approach and using the modeling aerodynamic interference as feedback nonlinearities, a new autopilot for uav close formation flight is designed

    採用全狀態量反饋,同時將氣動干擾作為非線性反饋,設計出一套適用於無人機近距離編隊飛行的自動駕駛儀
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