节点文献

基于MEMS技术的组合导航系统在空地制导武器中的应用

Application of MEMS-based integrated navigation system in aerial-to-ground guidance weapon

  • 推荐 CAJ下载
  • PDF下载
  • 不支持迅雷等下载工具,请取消加速工具后下载。

【作者】 王春陵; 华克强; 孙淑光;

【Author】 WANG Chun-ling1,HUA Ke-qiang2,SUN Shu-guang2 (1. Dalian TV University Brand College,Dalian 116300,China; 2. Aeronautical Automation College,Civil Aviation University of China ,Tianjin 300300,China)

【机构】 大连电视大学瓦房店分校数学教研室; 中国民航大学航空自动化学院; 中国民航大学航空自动化学院 大连116300; 天津300300;

【摘要】 针对空地精确制导武器对低成本、高精度、高可靠性导航系统的需求,设计了基于MEMS技术的组合导航系统。该系统基于低成本的微惯性测量组合与GPS接收机,并针对空地制导武器的飞行特点建立了准确的数学模型;利用速度、位置综合模式,采用先进的Kalman滤波理论进行数据融合;最后对该组合导航系统进行了数学仿真试验和数据分析。结果表明,这种低成本、可靠性好、体积小的组合导航系统的导航精度不大于5m,即使在丢星长达30s,导航精度也不大于12m,完全能够满足空地精确制导武器的导航要求。

【Abstract】 An integrated navigation system for aerial-to-ground guidance weapon was designed based on MEMS and GPS-OEM panel to meet its requirement for low-cost,high-precision and high-reliability. A precise mathematic model was set up based on Micro Inertial Measurement Unit/GPS and the weapon’s flying feature. Data fusion was implemented using Kalman filter with position and velocity as measurement variables. The mathematical simulation and data analysis were made to test the performance of the integrated navigation system. The results show that the low-cost integrated navigation system is less than 5 m in accuracy for up to 30 s interrupted time,and navigation accuracy is less than 12 m. So it can work with better precision and perfect reliability.

  • 【文献出处】 中国惯性技术学报 ,Journal of Chinese Inertial Technology , 编辑部邮箱 ,2007年03期
  • 【分类号】TJ762.21
  • 【被引频次】15
  • 【下载频次】512
节点文献中: 

本文链接的文献网络图示:

本文的引文网络