期刊文献+

超小型无人机GPS/MIMU组合导航定位系统研究 被引量:4

Study of GPS/MIMU Integrated Navigation and Location Systems for SUAV
下载PDF
导出
摘要 在考虑超小型无人机特点及其对导航定位需求的基础上,研究了利用微型惯性测量单元(MIMU)和GPS-OEM板,设计出一种低成本、轻小型的GPS/MIMU组合导航定位系统。为了验证该系统的性能,利用MIMU和GPS观测数据对该组合系统进行了仿真。仿真结果表明,组合导航系统在精度和可靠性方面,较单一的导航系统都有明显的改善。 Based on the characteristic and the demands for navigation and location to SUAV, a low cost GPS/MIMU integrated navigation system is designed by using MIMU and GPS-OEM panel in this paper. In order to verify the performance of the integrated system, the simulation is implemented by using the actual data measured and observed. The simulation results show that the integrated navigation system can more greatly improve reliability and precision than the single navigation system.
出处 《航空电子技术》 2004年第3期15-18,34,共5页 Avionics Technology
关键词 超小型无人机 微型惯性测量单元 GPS/MIMU 组合导航 Super-mini Unmanned Aerial Vehicle Micro-miniature inertial sensor GPS/MIMU Integrated navigation
  • 相关文献

参考文献1

  • 1Silva R N, Murray G W. Low cost quartz rate sensors applied to tactical guidance IMUs [C]. Proceeding of the IEEE Position,Location and Navigation Symposium, 1994: 37-42.

同被引文献29

引证文献4

二级引证文献6

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部