宇航计测技术 ›› 2015, Vol. 35 ›› Issue (4): 54-57.doi: 10.12060/j.issn.1000-7202.2015.04.12

• 论文 • 上一篇    下一篇

RNSS/INS深耦合高动态导航接收机测试方法研究

王田1;张书锋1;张明志1;彭明1;陈强1;张于1   

  1. 1、北京东方计量测试研究所,北京 100094
  • 出版日期:2015-08-15 发布日期:2015-08-15
  • 作者简介:王田(1990-),男,硕士研究生,主要研究方向:卫星导航测试研究。

Study on Test Methods of RNSS/INS Deeply Coupled Integrated High Dynamic Navigation Receiver

WANG Tian1;ZHANG Shu-feng1;ZHANG Ming-zhi1;PENG Ming1;CHEN Qiang1;ZHANG Yu1   

  1. 1、Beijing Orient Institute for Measurement, Beijing 100094
  • Online:2015-08-15 Published:2015-08-15

摘要: 卫星导航和惯性导航采用深耦合方式实现导航作为世界上最先进的导航形式,在国防中的应用越来越广泛,但其在高动态下的性能需要验证。当前针对深耦合高动态下导航接收机的测试研究较少,本文介绍了基于卫星信号模拟器的测试系统组成及测试用高动态场景,运用模拟测试原理,通过对导航接收机在高动态下定位速度和跟踪灵敏度的测试及其结果分析,验证了导航接收机的深耦合功能,对此类接收机的测试方法进行了初步探究。

关键词: 深耦合, 高动态, 导航接收机, 测试方法

Abstract: The satellite navigation and inertial navigation of using deeply coupled are the world′s most advanced navigation form. With more and more wide application in defense, its performance in high dynamic state needs to be verified. There is a lack of study on test of deeply coupled receiver under high dynamic state at the moment. The composition of test systems based on satellite signal simulator and the test high dynamic authentication are described. The deeply coupled function of navigation receiver is verified through testing location velocity and tracking sensitivity under high dynamic authentication and its analyzing their messurement results, a preliminary study on the navigation receiver test methods based on satellite signal simulator is presented.

Key words: Deeply coupled, High dynamic state, Navigation receiver, Test method