宇航计测技术 ›› 2014, Vol. 34 ›› Issue (4): 29-32.doi: 10.12060/j.issn.1000-7202.2014.04.07

• 论文 • 上一篇    下一篇

车载惯导校准装置仿真测试系统的设计与研究

刘华1；张璁1；唐声权1   

  1. 1、北京航天计量测试技术研究所，北京 100076
  • 出版日期:2014-08-15 发布日期:2014-08-15
  • 作者简介:刘华（1983-），男，工程师，主要研究方向：惯导测试设备、稳定跟踪设备及仿真设备。

Design and realization of testing and simulation system of Calibration Device for Inertial Navigation in Vehicle

LIU Hua1；ZHANG Cong1；TANG Sheng-quan1   

  1. 1、Beijing Aerospace Institute for Metrology and Measurement Technology,Beijing 100076
  • Online:2014-08-15 Published:2014-08-15

PDF (PC)

摘要： 为了提高车载惯导校准装置系统的通用性和易扩展性,使该平台能够对不同型号的惯导系统进行测试，研究与设计了一套仿真测试系统软件。介绍了该系统的整体结构，并按功能将设计分为测试系统和仿真系统两部分,详细说明了这两部分的实现方法。实施结果表明,通过这种软件平台搭建的系统，具有实时性强、算法运行可靠、结构紧凑、操作简单的特点。

关键词: 车载惯导, 校准装置, 仿真软件, 测试

Abstract: In order to enhance the universal ability and expandability of inertial navigation testing system in vehicle, and inertial navigation of different kind could be tested in the same platform, a new inertial navigation testing and simulation system software is researched and designed. Components and structure of the system are introduced briefly in this paper. Due to the function of this system,the framework is divided into two parts,testing system and simulation system.Each part approach of realization is interpreted in detail. At the end the practice shows that this whole system has the characteristics of  strong realtime, stable operation and easy using.

Key words: Inertial navigation system in vehicle, Calibration device, Simulation software, Testing

京ICP备09048426号-4　 京公网安备 11010602060144号　版权所有 © 《宇航计测技术》编辑部