In view of engineering utility and maintenance, an in-flight calibration method for aircraft SINS was presented.
从工程实用和维护的角度出发，提出了一种针对机载捷联式系统的空中标定方法。
The locating, installation and calibration of stall warning device are all determined by the experiment in flight test.
失速警告器的选位安装与校准均由试飞实验确定。
Meanwhile, simultaneity of different flight path data can be realized via time calibration arithmetic.
同时，采用时间对准算法实现不同航迹数据的同时性。
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