姿態修正 的英文怎麼說

中文拼音 [tàixiūzhēng]
姿態修正 英文
attitude correction
  • 姿 : 名詞1. (容貌) appearance; looks; mien; aspect 2. (姿勢) gesture; carriage; bearing
  • : 名詞1. (形狀; 狀態) form; condition; appearance 2. [物理學] (物質結構的狀態或階段) state 3. [語言學] (一種語法范疇) voice
  • : Ⅰ動詞1 (修飾) embellish; decorate 2 (修理; 整治) repair; mend; overhaul 3 (寫; 編寫) write;...
  • : 正名詞(正月) the first month of the lunar year; the first moon
  1. Using piezoresistive accelerometers and magnetoresistance sensors measure the dynamic acceleration and geomagnetic field and through avr mcu software to calculate the attitude angular and azimuth. the fact of affecting the module is discussed in detail in this report and put forward the resolving scheme of key technology of digital filter, linear compensation, temperature compensation and magnetic field adjustment. the digital module has advantages of small size, light weight, low conception, high accuracy, all solid state and high reliability

    本課題採用壓阻式加速度計和磁阻傳感器分別測量重力加速度和地磁場,通過avrmcu軟體解算出姿角和方位角,課題詳細分析了影響模塊性能指標的因素,就數字濾波、線性補償、溫度補償、磁場等關鍵的技術問題提出了可行的解決方案,研製的數字化模塊具有體積小、重量輕、低功耗、精度高、全固、高可靠等特點,所有性能指標均滿足設計要求,為姿角測量提供了有效的手段。
  2. In the attitude determination experiment, star sensor hardware is introduced into the control loop to correct the gyro bias. in the attitude control experiment, firstly using reaction thrusters to perform large - angle slew and then

    姿確定實驗中引入星敏感器實物到控制迴路中對陀螺數學模型中的漂移進行;姿控制實驗中先進行噴氣大角度控制後用飛輪進行穩定控制。
  3. The method can eliminate the conventional fuzzy control system ' s steady - state errors and flutters. considering wind disturbance, the stabilized loop of pitch angle was designed and simulated with this method

    9採用帶優化函數無量化的模糊控制方法設計國產直九c海豚直升機的縱向姿角穩定迴路系統。
  4. Mode 1 is for gross attitude correction, and is the closest thing the craft has to a safe mode

    模式1為姿態修正,也是讓航空器能夠進入一個安全狀的關鍵模式。
  5. Firstly, making out the walking poses and tracks of the robot, according to the study on the humans ’ gait and the sine and cosine curves are used to program its center - of - gravity track and its feet - lifting track. secondly, the kinematics model is established, and according to the constraint and the programmed tracks, the kinematics equations of each walking stages are available. then find the solutions of each equation and get the motion curves of its joints, which are also the motion curves of the mini - servomotor

    首先,結合對人類行走步的研究,規劃機器人行走姿及軌跡;在此基礎上建立並求解運動學方程,獲得機器人行走時各關節的轉角曲線;最後,針對前向運動與側向運動之間的耦合,對求得的運動曲線進行,使機器人在保證穩定的前提下,動作更加流暢。
  6. Furthermore, it is insure that the carrier pahse measurement data does not have cycle slips in gps based attitude determination system, using phase rate prediction algorithm and baseline length constraint information algorithm, the cycle slips can be detected and corrected successfully, which markedly reduce the initialization numbers of attitude determination system

    此外,在gps姿測量系統中,必須保證載波相位觀測數據中無載波相位周跳,本文提出的多普勒預測演算法和基線長度約束相結合的方法能有效的檢測和載波相位整周模糊值固定前和固定后的周跳問題,減少了姿測量系統重新初始化的次數。
  7. Using gyro measurements during periods of thruster firing, with thruster outputs, mass property identification is achieved through recursive least squares algorithms on the basis of the refined dynamics equation. the approach addresses the issue by segmenting the problem into two sub - problems which both allow closed form solution to reduce computation load

    該方法利用衛星上的陀螺輸出和推力器控制指令作為演算法的輸入,在的衛星姿動力學模型基礎上,推導了衛星質量特性在線辨識遞推最小二乘演算法,將質心位置和轉動慣量矩陣的辨識解耦以降低辨識演算法的維數,減少計算量。
  8. The system would rely on active balancing and thus be “ dynamically stable ” ? that is, it would remain erect only if it made continual corrections to its body attitude

    這套系統採用主動式平衡裝置,可達到所謂的動穩定,也就是它必須不斷姿勢,才能維持站立狀
  9. This paper studied zero - velocity correct technology for ins, based on analysis of ins error equation, it concluded the method by which we can use ins velocity output to estimate the attitude angle error when the vehicle halted, then it contrasted two schemes of conic approximation of attitude angle error and put forward a method to decide the approximation coefficient by time range

    本文首先研究了車載捷聯慣導系統( ins )的零速技術,在分析捷聯慣導系統誤差方程特點的基礎上,推導了停車時利用ins速度輸出估計姿誤差角的方法,並對用二次曲線擬合姿誤差角的兩種方案作了比較,提出了按時間分段確定擬合系數的方法。
  10. It ' s inclined to the plaintiff or the defendant ? this text regards development of the american - european product liability law as the basis, attempt to use the menthods, such as, analytic approach of value, historical analytic approach, the case kw and comparative law, etc. analysing and probing into its theoretical foundation and value orientation, we should not only adhere to the modification of concrete clause, nor imitate foreign blindly, but really understand its marrow, guide the practise of legislation and justice of our country. develop and perfect the product liability law of our country further, hold the equalization points of justice and efficiency, rights and function correctly

    透過法律條文的表面去探求制度深層的必然性和內在的基本使命,本文以歐美產品責任法的發展為依據,試圖運用價值分析法、歷史分析法、判例法和比較法等方法,分析探討產品責任制度的理論基礎和具體內容,尤其是制度立足其上的理論基礎和價值取向,這樣才能站在理性的高度從宏觀去把握,以一種開放的姿去面對現實的挑戰,而不是僅僅拘泥於對具體條文的改,也不是盲目的照般國外的,真領會歐美產品責任制度的精髓,並以此來指導我國的立法和司法實踐,進一步發展和完善我國的產品責任法,確把握公平與效率、權利和功用的平衡點。
  11. Attitude error correction method of measurement of aircraft fuel

    飛機燃油油量測量及姿誤差方法
  12. Various attitude algorithm for strap - down inertial navigation system are studied. under the condition of coning movement, the contrast simulation of tow kind attitude algorithm is done

    研究了捷聯慣導系統各種姿矩陣的方法,並對其中的兩種方法在典型圓錐運動的條件下進行了對比模擬研究。
  13. In addition, with the gyro and the help of the modified rodrigues parameters ( mrps ), the proposed method can make the unit norm constraint on quaternion be satisfied

    在有陀螺模式下,設計了基於誤差羅德里格參數( mrps )的sukf姿估計演算法,在計算過程中同時能夠保證四元數始終歸一化。
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