Characterization of Inter Constellation Bias between NavIC and GPS and Methods for Performance Improvement in Positioning

S. VinojV., C. RadhakrishnaPillai, T. AnandShankarO., A. MohammedBasim, S. BijuV., Aneesh K Thampi, S. Sasikumar, D. Dev
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Abstract

The introduction of new navigation satellite constellations has opened up tremendous opportunity for commercial receivers to utilize larger number of satellite measurements for positioning. Generally, in these receivers, inter constellation bias (ICB) is treated as an unknown parameter and is estimated along with computation of solution. The accurate estimation of ICB prior to execution of positioning algorithm can enhance the solution availability of multi constellation receivers in GNSS scarce environment. This is particularly useful for terrestrial receivers which operate in dense forests, urban canyons and high dynamic receivers used in launch vehicle applications. As a special case, the behavior of ICB between GPS and NavIC constellations is studied in this paper. The objective of this work is to generate a reliable and fairly accurate model of the Inter-Constellation Bias (ICB) between GPS and NavIC system. This model can be used to estimate the value of ICB for a short duration and its usage enables the receiver to use a minimum number of satellites (lowest possible number being 4) from GPS and NavIC constellations for accurate positioning in a GNSS scarce environment. It is possible to generate reliable solution with good PDOP using five or six satellites, whereas the conventional method of ICB estimation along with position computation requires one more satellite and may result in relatively poor PDOP under GNSS scarce environment. In this study, ICB between GPS and NavIC constellation is estimated using NavIC and GPS independent navigation solutions computed over Indian region (Thiruvananthapuram, India- Lat: 8.53522°, Long: 76.9929°) for more than a year. The estimation is done using three independent GNSS Receivers: M/s NovAtel make, M/s Accord make and in house developed high dynamic GNSS Receiver. The overall characterization of ICB variation is carried out and further fine refinements are being attempted. Fine resolution data samples of one second and coarse resolution data samples of one day is used for short term and long-term characterization of ICB. The navigation computation is done using predicted ICB from the model. The obtained results are excellent and closely matching with the conventional algorithm which uses ICB as one of the unknown parameters in position computation.
NavIC与GPS星座间偏置特性及定位性能改进方法
新的导航卫星星座的引入为商业接收机利用更多的卫星测量值进行定位提供了巨大的机会。在这些接收机中,通常将星座间偏置(ICB)作为一个未知参数,在求解的同时进行估计。在执行定位算法之前对ICB进行准确估计,可以提高GNSS紧缺环境下多星座接收机解的可用性。这对于在茂密森林、城市峡谷和运载火箭应用中使用的高动态接收器中工作的地面接收器特别有用。作为一种特殊情况,本文研究了GPS和NavIC星座之间的ICB行为。这项工作的目的是生成一个可靠的和相当准确的GPS和NavIC系统之间的星座间偏差(ICB)模型。该模型可用于在短时间内估计ICB的价值,它的使用使接收机能够在GNSS稀缺的环境中使用来自GPS和NavIC星座的最少卫星数量(最低可能数量为4颗)进行精确定位。利用5颗或6颗卫星就可以得到具有良好PDOP的可靠解,而传统的ICB估计和位置计算方法需要多一颗卫星,在GNSS稀缺环境下可能导致PDOP相对较差。在本研究中,使用NavIC和GPS独立导航解在印度地区(Thiruvananthapuram, India- Lat: 8.53522°,Long: 76.9929°)计算了一年多的GPS和NavIC星座之间的ICB。利用三个独立的GNSS接收机:NovAtel、Accord和自主研制的高动态GNSS接收机进行估计。对ICB变化进行了全面表征,并正在尝试进一步细化。采用1秒的精细分辨率数据样本和1天的粗分辨率数据样本进行ICB的短期和长期表征。利用模型预测的ICB进行导航计算。所得到的结果与将ICB作为未知参数之一进行位置计算的传统算法吻合较好。
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