摘要
由于动基座的非匀速运动,给惯导系统平台的调平带来了附加误差。通过分析动基座在水平方向的运动加速度,推出了惯导系统平台调平等效误差角模型,并给出了一种快速初始对准方案。
The unevenly movement of the moving base causes the additional error in adjustment of Inertial Navigation System（INS） platform.The horizontal acceleration of the moving base was analyzed in this article,and the model of equivalent error angle adjustment of INS was deduced.The concept that can realize Rapid Initial Alignment was brought forward.
出处
《导弹与航天运载技术》
北大核心
2010年第5期12-14,共3页
Missiles and Space Vehicles
