基于UWB到达时间差的暗室高速定位测试方法研究

Research on Testing Method of High-Speed Positioning Based on TDOA of UWB in Darkroom

  • 摘要: 针对高落速云爆弹(FAE)二次引信与燃料云团交会最佳起爆位置控制困难,交会位置验证手段不足的问题,开展基于超宽带(UWB)的二次引信炸点定位测试研究。以二次引信标签与地面基站测距信息、基站间同步与测距时间差信息构建基于到达时间差(TDOA)的FAE二次引信炸点定位测试模型,并利用Taylor算法得到最优估计位置;提出基于拓展卡尔曼滤波(EKF)的炸点动态定位优化算法,实现位置修正并进行仿真对比分析。结果表明:TDOA三边测量定位的EKF算法动态性能优于基于距离的EKF算法,定位误差不大于0.5 m。进行了暗室高速试验,搭建基站数量为8个、布局空间最大为10 m×5.8 m×18 m的UWB定位与测距试验环境,并进行了工程实现上的改进优化设计,实现了高动态二次引信炸点位置解算误差不大于0.391 m的效果。结果充分表明提出的定位测试方法的可行性,为后期FAE二次引信最佳起爆点控制的深入测试研究提供思路和验证手段。

     

    Abstract: In response to the difficulty in controlling the optimal intersection detonation position between the high falling speed fuel air explosive (FAE) secondary fuze and the fuel cloud cluster, as well as the insufficient verification methods for the intersection position, a study on FAE secondary fuze detonation point positioning testing based on ultra wide band (UWB) was carried out. A FAE secondary fuze detonation point positioning testing model based on time difference of arrival (TDOA) was constructed using ranging information between secondary fuze tags and ground base stations, and synchronization among base stations as well as ranging time difference information. And Taylor algorithm for calculation was used to obtain the optimal estimated position; a dynamic positioning optimization algorithm for secondary fuze detonation points based on EKF (extended Kalman filter) was proposed to implement position correction, and simulation comparison analysis was conducted. The results showed that the dynamic performance of the EKF algorithm based on TDOA trilateration positioning was superior to that based on distance, with a positioning error of no more than 0.5 m. High-speed experiments were conducted in the darkroom, the UWB positioning and ranging test environment with 8 base stations and a maximum layout space of 10 m×5.8 m×18 m was set up, and designs in engineering implementation were improved and optimized. The effect of achieving a high dynamic secondary fuze detonation point position calculation error of no more than 0.391 m fully demonstrates the feasibility of the proposed positioning testing method, providing ideas and verification methods for further testing research on FAE secondary fuze detonation point control in the later stage.

     

/

返回文章
返回