attitude determination 中文意思是什麼
attitude determination
解釋
姿態測定- attitude : n. 1. 姿勢，身段。2. 態度，看法。3. 【軍事】飛行姿態。4. 芭蕾舞的一個姿勢。
- determination : n. 1. 決心，決意。2. 決定，確定。3. 傾向。4. 【法律】判決；（權利的）消失，終止。5. 【物理學】測定，鑒定。6. 【邏輯學】規定，限定。7. 【醫學】（血的）涌集。
-
Experiment on gps based high - accuracy attitude determination
精密定向研究的實驗 -
In the base of rigid body kinematics, the equations of attitude computation was developed via the imu sensor ’ s output, and a new method of the integrated attitude determination using gyroscope ’ s dynamic output and accelerometer ’ s static output was presented
基於剛體運動學，本文給出了由慣性測量單元的輸出所確定的氣浮臺姿態解算方程，並提出了利用陀螺儀的動態輸出與加速度計的靜態輸出進行組合的姿態確定方法。 -
Integer ambiguity resolution is the key problem of gps based real - time attitude determination system which use double differencing carrier phase observables
Gps姿態測量通常採用雙差載波相位觀測量，因此整周模糊值解算成為gps實時姿態測量的關鍵問題。 -
Most of error sources can be eliminated by double differencing due to the short antenna seperations within gps based attitude determination system, multipath is the dominant error source
Gps姿態測量中，大部分誤差源可通過雙差得到抑制或降低，多徑誤差成為主要的誤差源。 -
With the rapid development of the carrier phase differencing technique and digital signal processing hardware, it is possible to implement real - time processing of gps based attitude determination system
隨著載波相位差分技術和數字信號處理硬體的快速發展， gps姿態測量的實時處理成為可能。 -
This thesis has researched the design and control of a new triaxial air - bearing experimental system. in this thesis, the attitude determination and the attitude dynamics and control of the system was focused on
本文對新型的三軸氣浮轉臺進行了設計與控制研究，重點研究了系統的姿態確定及動力學與控制問題。 -
Speed - precision measurement for high - accuracy logbased on gps attitude determination system
姿態測量系統在高精度計程儀速度標定中的應用 -
Designed semi - physical simulations emphasized on attitude determination algorithm based on star sensor combined with gyroscope, bang - off - bang time - optimal jet control algorithm, and quaternion feedback control algorithm using flywheel
重點針對星敏感器和速率陀螺聯合定姿演算法、噴氣bang - off - bang時間最優控制律演算法、反作用飛輪四元數反饋穩態控制律演算法分別設計了半物理模擬實驗。 -
The result shows that the solar radiation pressure moments play a mainly part. based on kalman filtering, three kinds of attitude determination algorithms were studied using the attitude sensor now available on the explorer : the first based on digital solar sensor ( dss ) and gyroscope when the star sensor is not available ; another based on dss, high - gain antenna ( hga ) and gyroscope when the explorer is in the earth - safe mode ; the third based on star sensor combined with gyroscope when the explorer is in the normal mode
針對配置了典型測量敏感器的深空探測器，基於擴展kalman濾波給出了其姿態確定的方法:針對星敏感器不可用情形，給出了使用太陽敏感器和速率陀螺定姿的濾波器演算法;針對安全模式下的對地穩定定向情形，給出了太陽敏感器和高增益天線融合速率陀螺信息的定姿演算法;針對正常巡航模式給出星敏感器和速率陀螺聯合定姿演算法。 -
Chapter studies attitude determination problem by multi - antenna. the coordinate system and ad - algorithm is introduced firstly
第三章研究衛星導航系統中多天線姿態確定問題。 -
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
姿態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修正;姿態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。 -
Last step is overall adjustment by using multi - epoch absolute and relative results of positioning and timing, in order to improve precision of positioning and timing. ii. some problems about attitude determination and integrity ambiguity resolving by using gps carrier phase are discussed
本論文主要論述了利用星載偽距、載波相位觀測值（含gps和擴展gps ）進行編隊星座運動狀態（位置、姿態和鐘差）整體解算的有關問題。 -
Thirdly, based on the thought of motion - based ambiguity resolution, a bi - satellite attitude determination method using non - planar baselines is developed making full use of the satellites ’ geostationary property. focused on movement mode demands, the dissertation brings forward a method by large angle yawing movement accompanied with small angle pitch vibration to efficiently solve the rank deficiency problem of vehicle planar motion
再次，在基於運動解模糊的思想基礎上，充分利用北斗衛星對地靜止的特性，提出了一種非共面基線的雙星定姿方法，並重點分析了對運動特性的要求，提出通過伴隨小幅俯仰擾動的大角度偏航運動方式來有效解決載體平面運動的觀測矩陣秩虧問題。 -
In this dissertation, the theory and realiztion of gps based attitude determination technique are studied, multipath effects on gps observables and carrier phase multipath mitigation are also analyzed
本文研究了gps實時姿態測量技術的理論及實現，並分析了多徑效應對gps觀測量的影響及載波相位多徑誤差抑制。 -
Based on extended kalman filter ( ekf ) algorithm, an traditional attitude determination scheme using star sensors and gyros was studied, and proved not able to achieve the required precision. so a new idea called instrument - in - loop was presented what using the attitude information contained in the payload ' s data for the control loop. the simulation proved that the instrument - in - loop method can greatly improve the precision of attitude determination with low cost
建立了svom衛星各種姿態敏感器的測量模型，研究了基於推廣卡爾曼濾波演算法的「星敏感器+光纖陀螺」定姿方案，指出了其無法滿足svom衛星的定姿精度要求，並提出了instrument - in - loop的思想，即利用衛星有效載荷測量數據中蘊含的高精度姿態信息來濾波定姿，從而在避免使用昂貴的星敏感器的同時大大提高了系統的定姿精度。 -
3. carry out the simulation of the kalman filter based on the gps / magnetometer attitude determination system and the ins / cns / infrared earth sensors attitude determination system. the results show that it can improve attitude determination accuracy by fusion theory
3 .利用聯邦kalman濾波演算法分別對採用gps 、磁強計和採用慣性陀螺、紅外地平儀、星敏感器的兩種衛星姿態確定方案進行了建模和模擬。 -
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姿態測量系統中，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修正載波相位整周模糊值固定前和固定后的周跳問題，減少了姿態測量系統重新初始化的次數。 -
A technique for gps attitude determination based on analytical method
基於解析法的全球定位系統姿態測量技術 -
In order to test the performance of the attitude determination and control methods presented in this thesis, the whole simulation loop of the small astronomical satellite ' s adcs was constructed
3 ）為了充分驗證本文提出的姿態確定和控制方法的效果，本文的最後建立了svom衛星姿控系統大迴路模型，並編寫了相應程序，進行了數學模擬。 -
Star sensor is a high accuracy instrument for attitude determination. the new generation of autonomous star sensor is characteristic with wider fov and higher accuracy as well as size, mass and power decreasing
星敏感器是一種高精度的姿態測量儀器，具有自主導航能力的新一代星敏感器的顯著特點是視場大，精度高，體積、質量、功耗不斷減小。
分享友人