flying attitude

Getting information of missile flying attitude is always one of the key characters during the study about accurate guidance weapon.

弹体飞行姿态信息的获取是现代化精确制导武器研究的关键技术之一。

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There are many methods to measurement the flying attitude, such as solar attitude angle sensor, high-speed photography and geomagnetic field sensor.

飞行体的姿态测试方法有许多种，如太阳方位角传感器遥测、高速摄影法、地磁传感器等。

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The paper research fire angle of the projectile, firing time of the rocket motor, assisted time of the rocket motor, flying attitude of the glide phase and the terminal phase guidance law to add the projectile firing range.

在建立的模型的基础上，深入研究了炮弹的射角、火箭发动机的点火时间、火箭发动机的助推时间、滑翔段的飞行姿态以及末段制导律等对炮弹的射程及性能的影响。

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Study on slider steady flying attitude in high density magnetic storage system

高密度磁记录系统中磁头稳定飞行状态研究

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