节点文献
SPKF滤波算法在紧耦合GPS/INS组合导航系统中的应用
Application of SPKF Algorithm for Tightly-coupled GPS/INS Integrated Navigation System
【摘要】 根据SPKF滤波理论,建立捷联惯导系统在地理坐标系中的误差方程和GPS导航定位的误差模型,设计了GPS/INS的SPKF滤波器。该系统中含有位置误差、速度误差、平台误差角、陀螺漂移、加速度计偏差等17维状态。利用伪距、伪距率的观测信息对全部状态进行观测。对组合导航系统进行了动态仿真,仿真结果表明系统估计状态的导航精度高,系统的鲁棒性好。
【Abstract】 According to the SPKF filter theory,this paper research on tightly-coupled GPS/INS integrated navigation system,which has 17 state of position error,velocity error,misalignment,gyro bias,accelerator bias.INS error equations projected in geographic coordinate and GPS error model are established,and SPKF filter model of GPS/INS is designed.Computer simulation results show that navigation accuracy is improved greatly,and the robust of system shows goodness.
【关键词】 GPS/INS组合导航;
紧耦合;
SPKF滤波;
导航精度;
【Key words】 GPS/INS integrated navigation; tightly-coupled; SPKF filter; navigation accuracy;
【Key words】 GPS/INS integrated navigation; tightly-coupled; SPKF filter; navigation accuracy;
【基金】 国家自然科学基金资助(60474046)
- 【文献出处】 弹箭与制导学报 ,Journal of Projectiles,Rockets,Missiles and Guidance , 编辑部邮箱 ,2007年01期
- 【分类号】V249.328
- 【被引频次】6
- 【下载频次】508