首页> 外文期刊>Procedia Computer Science >Elevation and Position Uncertainty based KF Model for Position Accuracy Improvement
【24h】

Elevation and Position Uncertainty based KF Model for Position Accuracy Improvement

机译:基于高度和位置不确定性的KF模型,用于定位准确性改进

获取原文
           

摘要

This paper discusses about improvement of Global Positioning System (GPS) receiver position accuracy based on elevation angle and position uncertainty parameters. Kalman Filter method is used to estimate the receiver position which by default provides position uncertainty along with error in position. To improve accuracy, the proposed method focuses on proper selection of satellites to be considered among the visible satellites to evaluate the receiver’s position accuracy. At a particular epoch the combination of satellites with high elevation angles results in better receiver position. The analysis has been carried out by considering different combinations of satellites with high elevation angles from a number of visible satellites at a particular epoch. The results of the proposed method are very promising for precise applications of GPS particularly in the civil aviation sector.
机译:本文探讨了基于仰角和位置不确定性参数的全球定位系统(GPS)接收机位置精度的改进。 Kalman滤波器方法用于估计接收器位置,默认情况下提供位置不确定性以及位置误差。 To improve accuracy, the proposed method focuses on proper selection of satellites to be considered among the visible satellites to evaluate the receiver’s position accuracy.在特定的时代,具有高仰角角度的卫星的组合导致更好的接收器位置。通过在特定时期的许多可见卫星中考虑具有高仰角的不同卫星的不同组合来进行分析。所提出的方法的结果非常有希望用于GPS的精确应用,特别是民用航空部门。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号