飛輪動量 的英文怎麼說

中文拼音 [fēilúndòngliáng]
飛輪動量 英文
fly wheel momentum
  • 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...
  • 輪 : Ⅰ名1 （輪子） wheel 2 （像輪子的東西） wheel like object; ring; disc 3 （輪船） steamer; steamboa...
  • 量 : 量動1. （度量） measure 2. （估量） estimate; size up
  1. Compress disk is the very important rotational component in the areoengine. when the compress disk is working, the grads of temperature and stress between the rim and the center of the disk are great. in order to raise the thrust - weight ratio of the disk and reduce oil consumption. the best prospective way is the dual alloys disk used

    壓氣機盤是航空發動機上一個很重要的轉動部件，壓氣機盤工作時，輪緣和輪轂溫度梯度和應力梯度較大，為了提高飛機發動機推重比、減低耗油量，要求壓氣機盤的工作溫度、使用性能更高，雙合金盤製造是最有發展前景的技術。
  2. 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，基於經典控制理論設計俯仰通道的pid控制律，根據滾動?偏航通道耦合的特點，分別討論了由軌道角頻率和章動頻率引起的長周期運動和短周期運動。其中長周期運動控制律設計時，結合了噴氣推力控制來輔助偏置動量控制;短周期運動控制中，為了解決不能獲得角速度信號的問題，採用terasaki提出的非最小相位控制器進行控制。
  3. Skate on the movement mechanics, materials science, and therefore must test equipment and technical strength of the company have more personnel and equipment, and therefore developed " flywheel licence skate " with its sophisticated quality, reasonable price and excellent brand reputation and win the favor of national 10, 000 ice - skating rinks, good reputation will help users " flywheel shoes " sweep away all obstacles

    溜冰鞋關繫到運動力學、材料科學，因此必須各種測試設備與技術力量，本公司具備以上人員與設備，因此所開發的「飛輪牌溜冰鞋」以其精良的品質、合理的價位、優良的品牌信譽，贏得全國近萬家溜冰場的青睞，良好的用戶口碑將有助「飛輪鞋」所向披靡。
  4. If electric actuators is used for power souce of the controling braking and hydraulic pressure of the plane, the system of hydraulic pressure woulde be cancelled or reduced. then the reliability and maintain woulde be increased and the weight of the plane woulde be minished

    採用電力作動器和功率電傳技術作為飛機操縱、環控、液壓、機輪剎車的動力源，減小或取消了集中式的液壓系統，可以使飛機的可靠性和維修性大大提高，重量大大降低。
  5. On the basis of reference ( superscript [ 6 ] ), the influence of damping of shimmy damper, moment of inertia of wheel, tire cornering stiffness and strut tilt stiffness on parametric shimmy stability of aircraft wheel is investigated in the paper

    摘要本文在文獻[ 6 ]的基礎上，首次研究了減擺器阻尼、機輪轉動慣量、輪胎偏滾剛度、支柱側傾剛度對飛機機輪參數擺振穩定性的影響。
  6. Under reading a lot of domestic and foreign study about flywheel battery, this paper is for the purpose of the application of the flywheel battery on the electric vehicle and uninterruptible power supply ( ups ). i complete the design of hardware and software about power electronics package conversion controller system of medium and small flywheel battery

    本論文在查閱了大量國內外相關研究的基礎上，以電動車輛和不間斷電源（ ups ）為應用背景，進行了中小功率飛輪電池的電力電子轉換控制系統的硬體電路和軟體設計。
  7. Firstly, i present a new structure of torque measurement ? rating torque sensor. secondly, introduce the fundamental principle of the dynamic torque. and then bring forward new methods of measuring flywheel moment and acceleration, which has been proved not only by theory, but also by experiment

    本文首先提出了轉矩測量的一種新結構? ?光柵靜態（平均）轉矩測量傳感器；然後闡述了動態轉矩測量的基本原理；接著提出了新的飛輪矩與加速度測量方法，並對其進行了理論推導及實驗證明；最後對提出的通用轉矩測量系統進行了硬體、軟體上的設計。
  8. Secondly, for satellite controlled by reaction wheels, an algorithm or strategy is presented. and then reaction wheels are used to generate a known disturbance torque, using thrusters as controller and gyro as the attitude sensor, a thruster parameters calibration for thruster levels and alignments on - line is achieved

    其次，針對反作用飛輪控制的衛星，提出了一種衛星質量特性在線辨識策略和辨識演算法，並利用反作用飛輪產生擾動力矩，推力器作為控制執行機構，使用陀螺測量衛星姿態角速度，實現推力器推力大小和方向等參數的在線辨識。
  9. Generally speaking, the algorithm of terrain contour matching is adapted to be used in cruise missiles which made fight path prior for that this algorithm is not a real - time system for it makes use of historical terrain data. while kalman filter algorithm is a real - time, rapid calculation system. which is appropriate for pilot or pilotless aircraft

    得出，地形輪廓匹配演算法使用歷史地形數據，實時性差，比較適合事先規劃好航跡的導彈使用：卡爾曼濾波的方法有較好的實時性，計算速度快，很適合有人無人駕駛飛機的機動飛行要求；小波分層只是對地形信息做了高低頻分解，其本質還是相似性度量演算法，但它有效的降低了匹配演算法的計算量。
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