›› 2014, Vol. 27 ›› Issue (1): 22-.

• 论文 • 上一篇    下一篇

面向紧耦合导航的伪距/伪距率高精度快速算法

尚煜,李耀军,张江华   

  1. (西安电子工程研究所 总体3部,陕西 西安 710100)
  • 出版日期:2014-01-15 发布日期:2014-01-12
  • 作者简介:尚煜(1988—),男,硕士研究生。研究方向:GPS/INS组合导航。E-mail:15829019325@163.com

Fast and Accurate Algorithm of Pseudo-range/pseudo-range Rate

 SHANG Yu, LI Yao-Jun, ZHANG Jiang-Hua   

  1. (Overall Unit 3,Xi'an Electronic Engineering Research Institute,Xi'an 710100,China)
  • Online:2014-01-15 Published:2014-01-12

摘要:

INS/GPS紧耦合导航中将卫星伪距、伪距率作为观测量,而伪距、伪距率中的误差影响了组合导航系统的输出精度,其运算量大,制约了紧耦合导航系统数据率的提高。文中通过实测数据探讨了紧耦合导航中伪距、伪距率的误差来源,并使用相对伪距、伪距率消除其中的接收机误差项。在此基础上提出利用Hermit分段3次插值法实现对卫星位置的快速解算,得到一种面向紧耦合导航的伪距、伪距率高精度快速估计算法。实验结果表明,该算法有效提高了伪距、伪距率的计算精度与速度。

关键词: 伪距, 相对伪距, Hermit插值

Abstract:

A tightly-coupled INS/GPS integrated navigation system is put forward which takes the pseudo-range and pseudo-range rate of GPS as the observations.Errors of pseudo-range affect the integrated navigation system output accuracy,and the large computation of computing pseudo-range and pseudo-range rate restrict the tightly coupled navigation system data rate.The sources of pseudo-range error and pseudo-range rate error are discussed.The error of receiver is eliminated by using relative pseudo-range and relative pseudo-range rate.On this basis,a fast and accurate algorithm by using Hermit piecewise cubic interpolation to solve pseudo-range and pseudo-range rate in tightly-coupled INS/GPS integrated navigation is studied.The experimental results indicate that the algorithm can improve the accuracy as well as the speed of solving pseudo-range and pseudo-range rate.

Key words: pseudo-range;relative pseudo-range;Hermit polynomial interpolation

中图分类号: 

  • TN967