| Kalman滤波技术在磁航向和捷联惯性组合系统初始对准中的应用 |
| |
| 引用本文： | 何秀凤,袁信,汪淑华. Kalman滤波技术在磁航向和捷联惯性组合系统初始对准中的应用[J]. 南京航空航天大学学报, 1995, 0(3) |
| |
| 作者姓名： | 何秀凤 袁信 汪淑华 |
| |
| 作者单位： | 南京航空航天大学自动控制系 |
| |
| 摘 要： | 研究了磁航向和捷形惯性组合系统初始对准的设计方法。该方法能在初始对准过程中用卡尔曼滤波器估计出陀螺仪的随机常值漂移，从而提高了系统的对准精度。文中给出了系统的状态方程和测量方程，建立了完全闭环控制的卡尔曼滤波器，最后给出了二组不同条件下的模拟结果。
|
| 关 键 词： | 惯性导航，卡尔曼滤波，对准，仿真 |
Application of Kalman Filtering to Alignment of Magnetic Heading and Strapdown inertial integrated System |
| |
| He Xiufeng, Yuan Xin, Wang Shuhua. Application of Kalman Filtering to Alignment of Magnetic Heading and Strapdown inertial integrated System[J]. Journal of Nanjing University of Aeronautics & Astronautics, 1995, 0(3) |
| |
| Authors: | He Xiufeng Yuan Xin Wang Shuhua |
| |
| Abstract: | Disscuss the alignment method of a magnetic heading and strapdown inertial integrated system. This method can estimate the random constant drifts of gyros,so that a high alignment accuracy of the integrated system is achieved. Give the error model of the integrated system. The algorithm of the closed-loop control Kalman filtering is established. Several simulation results under different conditions are shown. |
| |
| Keywords: | inertial navigation Kalman filtering alignment simulation |
| 本文献已被 CNKI 等数据库收录！ |
