论文部分内容阅读
提出了一种利用低成本捷联惯性系统的测量数据，对滚转的火箭或导弹弹体在弹道上受到的干扰因素进行辨识和根据这一辨识结果对飞行偏差进行预测的原理。在这原理基础上发展的技术，可用于对飞行过程的监测，也可用于火箭的制导。
A principle of using the measurement data of low cost strapdown inertial system to identify the disturbance factors of ballistic rocket or missile projectile on the trajectory and predicting the flight deviation based on the identification results is presented. The technology developed on the basis of this principle can be used for the monitoring of the flight process as well as for the guidance of rockets.