Satellite availability and positioning performance of uncombined precise point positioning using BeiDou-2 and BeiDou-3 multi-frequency signals

To realize the smooth transition from regional BeiDou Navigation Satellite System (BDS-2) to the global one (BDS-3), the integration of BDS-2 and BDS-3 is important for providing continuous, stable and reliable positioning, navigation and timing (PNT) services for global users. This work used 154 globally distributed multi-GNSS (Global Navigation Satellite System) experiment stations spanning 30 days to analyze the satellite availability and positioning performance of uncombined precise point positioning (UC-PPP) under current BDS-2 and BDS-3 constellations. We focused on three issues: the influence of BDS-3 receiver tracking abilities, the positioning performance among different areas, and the benefit of multi-frequency observations. The results show that the elliptical zone caused by poor BDS-2 satellite visibility is disappeared when the evenly distributed BDS-3 medium earth orbit satellites are introduced. When BDS-3 are integrated with BDS-2, the area with the Position Dilution of Precision (PDOP) less than 2 can be expanded to 75° S-75° N and 30° E-150° W. The positioning performance of BDS-3 and BDS-2/BDS-3 UC-PPP are seriously affected by the receiver tracking abilities of BDS-3 signals. When the maximum pseudo-random noise sequences (PRNs) of BDS-3 satellites tracked by stations are within 30 or 37, the positioning accuracy of static UC-PPP can be improved by 22.94% or 8.27% due to the integration of BDS-2 and BDS-3. Besides, the most improvement of BDS-2 and BDS-3 integration is achieved in Asia-Pacific regions, especially for the kinematic UC-PPP or the poor receiver tracking abilities of BDS-3. Similar to the multi-frequency BDS-2 UC-PPP, the benefit of multi-frequency signals for BDS-3 or BDS-2/BDS-3 UC-PPP is also non-vital. The three-dimensional positioning accuracy of BDS-2/BDS-3 multi-frequency UC-PPP in static mode and kinematic mode are 2.24 cm and 5.39 cm, while the corresponding convergence time are 49.62 min and 73.80 min, respectively. Compared with BDS-2, both the positioning accuracy and the convergence time of BDS-2/BDS-3 joint UC-PPP are improved by approximately over 50%, which indicates that BDS-3 has a great potential to provide high-quality PNT services as other global navigation satellite systems.     

天地环境差异对航天器设备安装精度影响分析

文章分析了地面重力环境和在轨内压环境对不同位置和状态下的载人航天器陀螺组件及姿轨控敏感器设备安装精度的影响,并进行了试验验证,分析结果与试验数据一致性较好。研究结果显示:设备布局位置不同,其安装精度受环境差异的影响程度也不同;航天器在空载、垂直停放状态下,设备安装精度受地面重力环境影响较小;陀螺组件和姿轨控敏感器A的安装精度受在轨内压环境影响较小,在地面常压环境下的精测结果能够真实反映其在轨状态,而姿轨控敏感器B的安装精度受压力环境影响明显。以上结果可为航天器设备布局及精度测量工作提供借鉴。     

低功率水电弧加热发动机的初步研究

本文研究了以水为推进剂的电弧加热发动机。其中电弧加热发动机的流量为15mg/s、电流为8A,此时平均电压为80.5V、功率约为640W、平均推力为0.0975N,以此计算得到比冲为650s左右、效率为55%～60%。成功地验证了水做为电弧加热发动机的推进剂、产生推力的能力。     

ITERATIVE COMPUTATION METHOD FOR NONLINEAR FORCED VIBRATION EQUATION ON HELICOPTER MAIN ROTOR LOAD

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超精密磨削中的超硬砂轮修整技术

论述了超精密磨削中广泛应用的几种超硬砂轮修整技术,分析了它们的工作原理,特点和适用范围.     

用经验模式参数研究电离层发电机效应

本文利用MSIS-86和IRI-86模式的基本参数,求得热层风系和电导率的三维分布;继而从发电机理论得到了电离层电位及层电流密度在北半球的分布和变化。本研究将大量数据统计平均的大气模式参数与热层、电离层理论研究联系了起来。     

充气展开式结构在航天器中的应用

充气展开式结构是以柔性薄膜材料制造的可充气展开的一种新型结构,具有体积小、重量轻和成本低的特点。文章介绍了充气展开式结构的设计原理,以及充气展开式结构在航天器中的应用和研究现状,并对充气展开式结构需要解决的关键技术进行了分析,最后对其在我国航天活动中的应用进行了展望。     

稀疏孔径成像系统发展概况

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过渡领域高超声速圆柱绕流直接模拟

本文用直接模拟蒙特卡罗方法模拟了再入速度为７．５ｋｍ／ｓ,高度分别为８０、８５、９０ｋｍ,物壁是完全漫反射有限催化壁的圆柱绕流。在８０ｋｍ考察了壁面催化率的影响。