GPS/VISNAV integrated relative navigation and attitude determination system for ultra-close spacecraft formation flying

For the improvement of accuracy and better fault-tolerant performance, a global position system （GPS）/vision navigation （VISNAV） integrated relative navigation and attitude determination approach is presented for ultra-close spacecraft formation flying. Onboard GPS and VISNAV system are adopted and a federal Kalman filter architecture is used for the total navigation system design. Simulation results indicate that the integrated system can provide a total improvement of relative navigation and attitude estimation performance in accuracy and fault-tolerance.

A-SMGCS中的航迹关联设计与实现

针对民航先进场面引导与控制系统(A-SMGCS)下的多传感器航迹关联融合问题,提出一种快速的航迹关联方法。该方法与基于分布式的联邦卡尔曼滤波相结合,构成一种稳定可靠的系统结构,并结合场面监视传感器特性,达到效率与精度的平衡。仿真实验结果表明,该关联方法是有效可行的,且具有较高的精度和处理效率。

基于联邦Kalman滤波的INS/SAR/TRN组合导航系统

在分析惯性导航系统(INS)、合成孔径雷达(SAR)和地形匹配导航系统(TRN)各自特点的基础上,提出了INS/SAR/TRN组合导航系统的组合滤波方案,并建立了相应的组合导航系统数学模型。仿真结果表明,组合导航系统能大幅度提高导弹的导航精度,具有重要的实际意义。