[an error occurred while processing this directive] [an error occurred while processing this directive] [an error occurred while processing this directive]
[an error occurred while processing this directive]
相关技术

基于跟踪微分器的单天线DGPS定向测姿方法研究

  • 苏鑫 ,
  • 万彦辉 ,
  • 谢波
展开
  • 中国航天科技集团第16研究所,西安 710100

苏鑫(1983-),男,陕西渭南人,硕士研究生,研究方向:组合导航定位测姿。

收稿日期: 2010-06-29

  网络出版日期: 2025-05-30

The Research on Single-antenna DGPS Determination Attitude Method Based on Tracking-differentiator

  • SU Xin ,
  • WAN Yanhui ,
  • XIE Bo
Expand
  • The 16th Institute, China Aerospace Science and Technology Corporation, Xi’an 710100, China

Received date: 2010-06-29

  Online published: 2025-05-30

摘要

设计了基于跟踪微分器的单天线DGPS定向测姿方法,构造基于积分方法的跟踪微分器,并将其用于DGPS速度的滤波和微分处理,从而得到较精确的速度和加速度信息,通过对载体运动模型的分析和数学推导,得到计算载体姿态的方法。最后,给出了该方法在车载系统中的仿真,结果表明该方法可以提供有效的姿态信息,可以成为常规姿态测量系统的备份。

本文引用格式

苏鑫 , 万彦辉 , 谢波 . 基于跟踪微分器的单天线DGPS定向测姿方法研究[J]. 弹箭与制导学报, 2011 , 31(2) : 199 -201,204 . DOI: 10.15892/j.cnki.djzdxb.2011.02.005

Abstract

A single-antenna DGPS aiding attitude determination method was designed. A trackin-differentiator based on integral ap-proximation was constructed. Using the TD, the DGPS velocity data could be filtered to better precise velocity and be differed toprecise acceleration. By analyzing the kinetic model of body and establishing the mathematic model, the solution procedure of atti-tude determination using the velocity and acceleration of body was presented. In the end, the process of simulation of the solutionand the error of attitude curves in the simulation system were presented. Simulation results and relative conclusion were provided.The results show that the method provides a useful source of attitude information and consequently may be used as a backup atti-tude system in vehicle navigation.

[an error occurred while processing this directive]

参考文献

[1]
卢鸿谦, 贺杰, 黄显林,等. 单天线GPS/加速度计组合测姿方法研究[J]. 哈尔滨工程大学学报, 2006, 27(6): 854-856.
[2]
韩京清. 自抗扰控制技术[M]. 北京: 国防工业出版社, 2008.
[3]
Richard P Kornfeld, R John Hansman, John J Deyst. Single-antenna GPS-based aircraft attitude determination[J]. Navigation, 1998, 45(1): 51-60.
[4]
刘大军. 利用单天线 GPS确定载体姿态的研究[D]. 南京: 南京航空航天大学, 2002.
文章导航

/

[an error occurred while processing this directive]