陀螺仪温度试验与建模研究  

TEMPERATURE TEST AND MODELING RESEARCH OF GYROSCOPE

作　　者：徐丽娜[1] 邓正隆[1] 张广莹[1] 诸一江 吕锡仁 

机构地区：[1]哈尔滨工业大学控制工程系 [2]北京自动控制研究所

出　　处：《宇航学报》1999年第2期99-103,共5页Journal of Astronautics

摘　　要：本文阐述了陀螺仪温度试验系统的结构和特点，用该系统进行了某型陀螺仪的温度速率与位置试验，并在试验基础上建立了陀螺仪静态温度模型。The structure and features of a gyroscope's temperature test system is presented in this paper.Using the system,rate and position test about gyro temperature character has been carried out.On the base of the test,a static model of gyro temperature features has been studied and its practicability of project has been proved by compensate study.

关 键 词：陀螺漂移 温度试验 系统辨识 陀螺仪 建模 

分 类 号：V241.506[航空宇航科学与技术—飞行器设计]