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首页> 外文期刊>中国航空太空学会学刊. >Positioning Method Design by Triple Difference and Taylor Series Expansion Techniques
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Positioning Method Design by Triple Difference and Taylor Series Expansion Techniques

机译:定位方法设计通过三差和泰勒系列扩展技术

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In this research the relative positioning method based on carrier phase was studied. The position of receiver is obtained by using the triple differences of carrier phase for different times and different satellites, in which both the errors of satellite and receiver biases as well as ionosphere propagation delays were replaced by the first order power series approximation, and then solving the navigation equations by the recursive method to minimize the least-squared-error. This methodology was not studied in the past. By using the GPS simulator for positioning, one can see that the positioning accuracy is about centimeter level, so it can be used for the system of higher accuracy requirement.
机译:在本研究中,研究了基于载体相的相对定位方法。 通过使用不同时间和不同卫星的载流子相位的三重差异来获得接收器的位置,其中卫星和接收器偏差的误差以及电离层传播延迟被第一订单功率序列近似替换,然后求解 递归方法的导航方程最小化最小二乘误差。 过去没有研究这种方法。 通过使用GPS模拟器进行定位,可以看出定位精度约为厘米级,因此它可用于更高的精度要求。

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