Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
8132162 | Advances in Space Research | 2018 | 16 Pages |
Abstract
This paper presents a method of deriving the instrumental differential code biases (DCBs) of GPS satellites and dual frequency receivers. Considering that the total electron content (TEC) varies smoothly over a small area, one ionospheric pierce point (IPP) and four more nearby IPPs were selected to build an equation with a convolution algorithm. In addition, unknown DCB parameters were arranged into a set of equations with GPS observations in a day unit by assuming that DCBs do not vary within a day. Then, the DCBs of satellites and receivers were determined by solving the equation set with the least-squares fitting technique. The performance of this method is examined by applying it to 361â¯days in 2014 using the observation data from 1311 GPS Earth Observation Network (GEONET) receivers. The result was crosswise-compared with the DCB estimated by the mesh method and the IONEX products from the Center for Orbit Determination in Europe (CODE). The DCB values derived by this method agree with those of the mesh method and the CODE products, with biases of 0.091â¯ns and 0.321â¯ns, respectively. The convolution method's accuracy and stability were quite good and showed improvements over the mesh method.
Keywords
Related Topics
Physical Sciences and Engineering
Earth and Planetary Sciences
Space and Planetary Science
Authors
Qi Li, Guanyi Ma, Weijun Lu, Qingtao Wan, Jiangtao Fan, Xiaolan Wang, Jinghua Li, Changhua Li,