仰角控制 的英文怎麼說

中文拼音 [yǎngjiǎokòngzhì]
仰角控制 英文
elevation control
  • : Ⅰ動詞1 (臉向上) face upward 2 (敬慕) admire; respect; look up to 3 (依靠; 依賴) rely on ; d...
  • : 角Ⅰ名詞1 (牛、羊、 鹿等頭上長出的堅硬的東西) horn 2 (古時軍中吹的樂器) bugle; horn 3 (形狀像...
  • : 動詞1 (告發;控告) accuse; charge 2 (控制) control; dominate 3 (使容器口兒朝下 讓裏面的液體慢...
  • : Ⅰ動詞1 (製造) make; manufacture 2 (擬訂; 規定) draw up; establish 3 (用強力約束; 限定; 管束...
  • 仰角 : [數學] elevation; angle of elevation; angle of gradient; angle of altitude; [軍事] quadrant eleva...
  • 控制 : control; dominate; regulate; govern; manage; check; cybernate; manipulate; encraty; rule; rein; c...
  1. Searching satellite is to change the azimuth angle and pitching angle by making antenna circumrotate azimuth axis and pitching axis with controller, so antenna can point itself to different satellite according to the demands

    尋星就是通過器的使天線圍繞方位軸和俯軸旋轉,從而改變天線的方位和俯,使天線根據要求對準不同的衛星。
  2. The paper designed aerodynamic control system of pith and yaw channels and roll angle stabilization system, by using unsteady - state error follow - up control theory and state observation station theory in modern control theory

    本文使用現代理論中的無靜差跟蹤系統理論與狀態觀測器理論,設計了俯、偏航兩個通道的氣動力系統和滾轉穩定系統。
  3. Fixed camera fastening its interior is loaded with an electric motor, on installs the good camera after the level to be possible to adjust the angle which the camera deals with, after achieved the best surveillance effect may accept the automatic control regulator by the electric motor the signal precisely to move the localization in under the control signal function, the camera already may automatically carry on the horizontal scanning to monitor the region, also may in under the monitoring center attendant s operation the moving surveillance object input voltage : ac 24v 50 60hz, 110v 60hz, 220v 50 60hz external dimensions : 119mm 115mm is high the weight : 0. 9kg material : abs high strength casts takes shape the degrees rotation : level biggest : 350, vertical 90 may adjust the velocity of whirl : 5 second 4 seconds revolve the spacing : exterior spacing card tunable load : 7kg function input plug : 1

    Kl - 306室內水平雲臺是安裝,固定攝像機的支撐設備.它內部裝有一電動機,在水平雲臺上安裝好攝像機后可調整攝像機俯度,達到最好的監視效果后可由電動機接受來自器的信號精確地運行定位.在信號的作用下,雲臺攝像機既可自動進行水平掃描監視區域,也可在監中心值班人員的操縱下跟蹤監視對象
  4. Then in allusion to biased momentum wheel system, based on classical control system a pid controller was design about pitching channel. according to specialty of roll - yawing channel, this paper discuss long - time cycle movement and short - time cycle movement. when design the control method of long - time cycle movement, whiff thruster is used to assistant the control system. when design the control method of short - time cycle movemen, in order to sovle the problem of coundn ’ t abtain the angular velocity signal, nonminimum phase controller advanced by terasaki is used

    然後針對偏置動量飛輪系統,基於經典理論設計俯通道的pid律,根據滾動?偏航通道耦合的特點,分別討論了由軌道頻率和章動頻率引起的長周期運動和短周期運動。其中長周期運動律設計時,結合了噴氣推力來輔助偏置動量;短周期運動中,為了解決不能獲得速度信號的問題,採用terasaki提出的非最小相位器進行
  5. To solve the problems caused by the varieties of the missile dynamics with the difference of flight height, velocity and attitude angle in modeling the missile, in this thesis, the theory of variable structure model reference adaptive control is used to design a pitch channel autopilot based on a longitudinal missile model, the status equation using the measurable parameters of load and angular rate is established, and the methodology to choosing the reference model is discussed also, and the performance of the controller is analyzed by means of simulation

    為了解決攔截彈氣動參數隨飛行高度、速度、姿態的不同,變化范圍大,系統難以準確建模的困難,基於縱向平面攔截彈模型,採用模型參考變結構理論設計了俯通道姿復合系統,以可測量變量過載和速度作為狀態量建立了系統的狀態方程,討論了參考模型的選擇方法,並對系統的性能作了模擬分析。
  6. After introduced its task and construct of the controller of the homing gliding missile, the longitudinal and lateral motion equations are provided. a continuous fuzzy - pid control system combined the advantages of fuzzy control and pid control is presented, and could be guaranteed the stability of the system using popov stability criterion. the results of simulation show that the fuzzy - pid control is able to provide a better relative stability and robustness, also have better dynamic and static characteristics than the pure pid control

    將模糊和pid相結合,研究了一種基於模糊pid的連續器,利用波波夫穩定判據判定該器是漸進穩定的,並將其應用於導滑翔彈俯、偏航、滾轉穩定迴路中,設計模擬結果表明,該種連續器可使系統獲得很好的穩定性和魯棒性,動、靜態性能比單純pid都有較大提高。
  7. So, variable structure control theory is used in angle stabilization of roll, and model - following variable structure control theory is used in acceleration stabilization of pitch and yaw

    因此,本文採用了變結構理論設計傾斜穩定系統,採用了模型跟蹤變結構理論設計俯、偏航通道的加速度穩定迴路。
  8. The controller adopts tms320f240 dsp as its main control unit, using code wheel for angle measurement, using synchronous serial communications interface for the duplexing data communication between the controller and the upper computer, using rs - 232 interface for the communication between the pitch axis controller and the azimuth axis controller, and then developed the interface circuit to the motor driver

    根據器研製要求,提出總體方案。器採用dsp作為主單元,利用光電碼盤測,利用同步串列通信介面與上位機進行雙向數據通信,利用rs - 232介面進行俯軸和方位軸器之間的通信,並研製了與電機驅動器的介面電路。
  9. H means the river front construction, d means the distance between river front constructions and river bank, d " means the distance between river front construction and the river bank on the other side, a means the angle of the visual line from the spot near the river bank and horizon

    本文總結「濱河恆等式」 ,針對城市骨幹河流水系(河寬大於或等於40米)其空間圍合度。 h (濱河建築高度) , d (濱河建築離河岸距離) , d (濱河建築離河對岸距離) , (人在河邊看河對岸景物度) 。
  10. This paper, in advantage of modern control theories, designed the pitch control system and the altitude holding system of the x armed helicopter, and present digital simulation, coupling analysis, sensitivity analysis, system performance analysis under different input and initial condition

    本文應用現代理論設計了某型武裝直升機的俯仰角控制系統和高度保持系統,並進行了數字模擬、耦合分析、飛行狀態變化對系統性能的影響分析,及在不同輸入初始條件下的系統性能分析。
  11. It is very important for mechanism - phase scanning phased array radar to effective distribute energy and time in elevation

    摘要掃描能量有效分配對機相掃體陣雷達的設計十分重要。
  12. According to the theory of boundary layer control and aerodynamics of delta wing at medium attack angle, the generation mechanisms of rolling, pitching, yawing moments, which are produced by coupling between the microactuator array and boundary layer near the leading edge, have been discussed

    首先,結合空氣動力學的邊界層原理以及三翼在中等攻條件下的氣動特徵,詳細討論了微致動器陣列通過與前緣邊界層的耦合產生三翼翻滾、俯和偏航等力矩的機理。
  13. The switch logic between high thrust and low thrust, switch rule between ppc methed and qsc methed, and the switch maneuver between pitching and attacking in af are given

    給出了高水平推力和低水平推力的切換邏輯,相平面與準滑模律的切換準則和度反饋中俯和攻的切換策略。
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