摘要
从捷联惯性测量组合的数学模型开始,提出了一种惯测组合快速测试方法,进行了理论推导,合理编排了测试位置,得出了惯测组合陀螺仪及加速度计各性能参数的计算公式。使惯性测量组合单元测试更趋于简单、方便,提高了测试精度,更加便于部队使用。
This paper promotes a new type of fast testing method of strap-down inertial measuring system after whose mathematical model has been studied, and finally comes up with a set of formulas for the gyroscope and determining of parameters of accelerometers as a consequence of theoretical derivation and rationally decided test point. This work makes the task of unit test of inertial measuring system easier and more convenient, while increases its precision and the convenience to use.
出处
《弹箭与制导学报》
CSCD
北大核心
2007年第1期30-33,共4页
Journal of Projectiles,Rockets,Missiles and Guidance
关键词
惯性组合
测试
陀螺
加速度计
inertial measuring unit
testing
gyroscope
accelerometer
