摘要
从理论原理出发,论述了基于科里奥利力原理建立数学计算模型,通过电量转换得到相应的角速度参数。并利用飞行器搭载MEMES传感器的方式,实现将科里奥里力理论原理应用实践在现实飞行器角速度的测试工作中,获得飞行器瞬时角速度等飞行参数。
Based on the theoretical principles,this article discusses how to establish a mathematical calculation model based on the Coriolis force principle,and obtain the corresponding angular velocity parameters through the conversion of electricity.Using the method of the aircraft carrying the MEMES sensor,the principle of Coriolis force theory is applied in the test of the actual aircraft angular velocity,and the flight parameters such as the instantaneous angular velocity of the aircraft are obtained.
作者
马思宇
周鑫
宋歌
田晓旸
曹萌
Ma Siyu;Zhou Xin;Song Ge;Tian Xiaoyang;Cao Meng(China Academy of Lauch Vehicle Technology,Beijing 100076)
出处
《航天制造技术》
2020年第3期61-64,共4页
Aerospace Manufacturing Technology
