INS/GNSS组合导航的航空布撒器制导控制系统分析与设计

Analysis and Design of the INS/GNSS Integrated Navigation Aviation Cloth Scattering Guidance Control System

利用惯导系统和GPS各自的特点,分析设计了IN S/GN SS组合导航的航空布撒器制导控制系统,并对惯导系统的误差方程进行了分析,研究结果表明,它可有效地提高系统导航参数的估计精度和速度,满足航空布撒器远距离飞行时的制导精度要求。

Using respective characteristic of the inertial systems anal GPS ,analyzing and designing the INS/GNSS combined navigation aviation cloth scattering guidance control system, and analyzing the error equation of the inertial systems. The findings indicated, it may effectively enhance the estimate precision and speed of the system navigation parameter, satisfying the guidance accuracy request when the aviation cloth scattering has a long aviation.