The Compensation Methods of the Start-up Drift of Four Frequency Differential Laser Gyro
The start-up drift of four frequency differential laser gyro is of great importance in the fast launching occasions like missiles and fighter plane. This paper studies the characteristics of startup drift and presents two kinds of compensation methods. Based on the tradihonal mathematic model in terms of temperature, temperature changing rate and temperature gradient, the software compensation is done with the drift data. From the analysis of the physics mechanism of start-up drift, the hardware compensation is realized by adopting the corresponding technologies to control the specific physics parameters thermal changes which directly cause the start-up drift. Experiments show that software compensarion is of little use while hardware compensation is more suitable and effective.
Four frequency differential laser gyro Start-up drift Software compensation Hardware compensation
Yang Jianqiang Liao Dan Jin Xin Jia Xueqing
College of Opto-electronics Science and Engineering,National University of Defense Technology,Changs College of Opto-electronics Science and Engineering,National University of Defense Technology, Chang 91746 Troop,The peoples Liberation Army,Beijing,China Division of Science and Research, National University of Defense Technology,Changsha,China
国际会议
The 2nd IEEE International Conference on Advanced Computer Control(第二届先进计算机控制国际会议 ICACC 2010)
沈阳
英文
237-240
2010-03-27(万方平台首次上网日期,不代表论文的发表时间)