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基于星敏感器的捷联惯性导航系统的陀螺仪仿真

Simulating Gyro of Strapdown Inertial Navigation System Based on Star Sensor
作者:Wei GaoLei Zhang 作者单位:College of Automation Harbin Engineering University No.145,Nantong street,Harbin,China;College of Automation Harbin Engineering University No.145,Nantong street,Harbin,China 加工时间:2014-06-26 信息来源:科技报告(Other) 索取原文[5 页]
关键词:星敏感器;陀螺仪;捷联式惯性导航系统;角速度
摘 要:In inertial navigation system,gyro is used to measure the angular velocity of carrier relative to inertial space for achieve attitude matrix updated in real time.Gyro difficult to eliminate the error,results in strapdown inertial navigation system precision decrease with time.Star sensor is a high-precision attitude measuring instrument and don't require any priori information,the attitude date can be provided by star sensor.Thus,gyro is simulated by star sensor in order to improve the precision of strapdown inertial navigation system.
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