检索规则说明:AND代表“并且”;OR代表“或者”;NOT代表“不包含”;(注意必须大写,运算符两边需空一格)
检 索 范 例 :范例一: (K=图书馆学 OR K=情报学) AND A=范并思 范例二:J=计算机应用与软件 AND (U=C++ OR U=Basic) NOT M=Visual
作 者:阳明晔[1] 宋章启[1] 张学亮[1] 陈宇中[1]
机构地区:[1]国防科技大学光电科学与工程学院,湖南长沙410073
出 处:《国防科技大学学报》2014年第3期46-50,共5页Journal of National University of Defense Technology
摘 要:光纤陀螺的输入轴失准角温度变化特性是光纤陀螺惯性系统正交校准所面临的主要难题。提出了一种有效地消除输入轴失准角测量误差的测试方法;对三只椭圆环结构的光纤陀螺进行了输入轴失准角温度特性研究。结果表明,三只椭圆环光纤陀螺的输入轴失准角分布比较集中;此外,椭圆环光纤陀螺的输入轴失准角随着温度变化呈非单调的曲线变化,高温过程的变化速度相对较快。该结论对光纤陀螺环制作工艺的改进提供了测试依据,并有助于惯性系统正交校准的温度补偿技术研究。The temperature variation characteristic of the input axis misalignment angle of fiber optic gyro has become one of the key problems of orthogonal calibration of the fiber optic gyro inertia system.Firstly,a kind of measurement method,which can eliminate the measurement errors effectively,was presented.Then,the input axis misalignment angles of three fiber optic gyros with elliptical-structure optical fiber rings were measured.It is found that the three samples have similar input axis misalignment angles;the input axis misalignment angles vary non-monotonously with the changing of temperature;and the varying velocity is fast relatively in high temperature region.The results may be useful for improving the manufacturing technology of the fiber ring of the fiber optic gyro and will be helpful to prompt the temperature compensation technology of the orthogonal calibration in fiber optic gyro inertia system.
分 类 号:V241.5[航空宇航科学与技术—飞行器设计]
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在链接到云南高校图书馆文献保障联盟下载...
云南高校图书馆联盟文献共享服务平台 版权所有©
您的IP:216.73.216.249