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 of rocket derailment, a novel and intelligent test method for missile off-track attitude is proposed. The method is to place the gyroscope and data acquisition circuit inside the test projectile with the projectile, and then recover the acquisition system , Read the data from the computer and analyzed, and finally get the relevant parameters of the rocket launch disturbance, and focused on solving the data storage, maintenance and recovery and other issues.