摘要
本文讨论了一种动基座子惯导系统传递对准精度评估方法，提出利用INS或差分GPS等参考系统与被试系统组成一个弹载导航数据测试系统，采用卡尔曼最优平滑技术，通过飞行试验实时记录和事后处理测试系统导航数据，获取高精度导航定位与初始对准参数估计的方法。
This thesis discussed the evaluation method of moving base INS transfer aliment, and introduced using reference system, such as INS or DGPS etc, make up navigation testing system in missile with being tested system, using Kalman prime smoothing technology, through real-time record and data process afterwards for flying test, to get high precision navigation and position, and evaluation method of initial aliment.
出处
《导航》
2010年第4期37-41,共5页
