摘要
根据火箭弹离轨时的具体环境,提出一种弹离轨姿态的新颖的智能化测试方法,该方法是将陀螺及数据采集电路置于试验弹的内部随弹体飞行,而后将采集系统回收,由计算机读出数据并进行分析,最终获取火箭弹起始扰动的有关参数,并着重解决了数据存储、保持及回收等问题。
According to the specific environment when a rocket just leaves the track, an intelligent flying attitude test method is presented in this thesis. In this method, gyroscope and data acquisition system are fixed together into rocket, and they fly with the rocket. After restoring the system, the acquisited data are fed to a computer through the comunication interface. Finally, an application software is used to get the rocket flying attitude angals. The problems of data memory and procession are mainly discussed in this thesis.
出处
《测试技术学报》
1997年第3期17-20,共4页
Journal of Test and Measurement Technology
关键词
火箭弹
数据采集
压电陀螺
测试
rocket projectiles
data acquisition
gyroscopes
disturbances
