甚长基线干涉测量(very long baseline interferometry,VLBI)技术是深空探测器测定轨的方法之一,也是行星无线电科学研究的重要手段.VLBI相时延通过解算相关相位的整周模糊度解算出探测器的VLBI时延观测量,可有效地降低相位随机误差的影...甚长基线干涉测量(very long baseline interferometry,VLBI)技术是深空探测器测定轨的方法之一,也是行星无线电科学研究的重要手段.VLBI相时延通过解算相关相位的整周模糊度解算出探测器的VLBI时延观测量,可有效地降低相位随机误差的影响,从而提高时延测量的精度.本文论述了解算相位整周模糊度的条件和方法,给出相时延的解算方法,并分析比较了相时延与群时延的随机误差水平.以嫦娥二号(CE2)卫星飞往拉格朗日L2点的探测任务为例,求解了两个月内10次VLBI观测的相时延并分析了数据质量.相时延和群时延分别联合测速测距数据的定轨结果表明,在150万公里的距离上相时延用于探测器的定轨是可行的.展开更多
When satellite navigation receivers are equipped with multiple antennas, they can deliver attitude information. In previous researches, carrier phase differencing measurement equations were built in the earth-centered...When satellite navigation receivers are equipped with multiple antennas, they can deliver attitude information. In previous researches, carrier phase differencing measurement equations were built in the earth-centered, earth-fixed (ECEF) co- ordinate, and attitude angles could be obtained through the rotation matrix between the body frame (BF) and the local level frame (LLF). Different from the conventional methods, a hybrid algorithm is presented to resolve attitude parameters utilizing the single differencing (SD) carrier phase equations established in LLF. Assuming that the cycle integer ambiguity is known, the measure- ment equations have attitude analytical resolutions by using simultaneous single difference equations for two in-view satellites. In addition, the algorithm is capable of reducing the search integer space into countable 2D discrete points and the ambiguity function method (AFM) resolves the ambiguity function within the analytical solutions space. In the case of frequency division multiple access (FDMA) for the Russian Global Orbiting Navigation Satellite System (GLONASS), a receiver clock bias estimation is employed to evaluate its carrier phase. An evaluating variable and a weighted factor are introduced to assess the integer ambiguity initialization. By static and dynamic ground experiments, the results show that the proposed approach is effective, with enough accuracy and low computation. It can satisfy attitude determination in cases of GPS alone and combined with GLONASS.展开更多
文摘甚长基线干涉测量(very long baseline interferometry,VLBI)技术是深空探测器测定轨的方法之一,也是行星无线电科学研究的重要手段.VLBI相时延通过解算相关相位的整周模糊度解算出探测器的VLBI时延观测量,可有效地降低相位随机误差的影响,从而提高时延测量的精度.本文论述了解算相位整周模糊度的条件和方法,给出相时延的解算方法,并分析比较了相时延与群时延的随机误差水平.以嫦娥二号(CE2)卫星飞往拉格朗日L2点的探测任务为例,求解了两个月内10次VLBI观测的相时延并分析了数据质量.相时延和群时延分别联合测速测距数据的定轨结果表明,在150万公里的距离上相时延用于探测器的定轨是可行的.
文摘When satellite navigation receivers are equipped with multiple antennas, they can deliver attitude information. In previous researches, carrier phase differencing measurement equations were built in the earth-centered, earth-fixed (ECEF) co- ordinate, and attitude angles could be obtained through the rotation matrix between the body frame (BF) and the local level frame (LLF). Different from the conventional methods, a hybrid algorithm is presented to resolve attitude parameters utilizing the single differencing (SD) carrier phase equations established in LLF. Assuming that the cycle integer ambiguity is known, the measure- ment equations have attitude analytical resolutions by using simultaneous single difference equations for two in-view satellites. In addition, the algorithm is capable of reducing the search integer space into countable 2D discrete points and the ambiguity function method (AFM) resolves the ambiguity function within the analytical solutions space. In the case of frequency division multiple access (FDMA) for the Russian Global Orbiting Navigation Satellite System (GLONASS), a receiver clock bias estimation is employed to evaluate its carrier phase. An evaluating variable and a weighted factor are introduced to assess the integer ambiguity initialization. By static and dynamic ground experiments, the results show that the proposed approach is effective, with enough accuracy and low computation. It can satisfy attitude determination in cases of GPS alone and combined with GLONASS.
