摘要
针对目前在发射场应用的测试方法不能分离出陀螺仪不等弹性静态漂移系数的现状 ,通过对陀螺仪静态漂移系数的测试原理和试验方法进行分析 ,推导了完整分离公式 ,提出了可行的分离方法。该方法可完整地分离出惯性平台陀螺仪各项静态漂移系数。
Aimed at the actuality that Different Elasticity drift coeflficient of gyroscope can't be separated by test method used in launching site at present, this paper analyzes experimental method and test theory of gyroscope static drift coefficient, deduces a complete separate formula and presents a practicable test method. Gyroscope static drift coefficient of inertial platform can be separated wholly by using the method.
出处
《上海航天》
2002年第1期36-38,共3页
Aerospace Shanghai
