首页 | 本学科首页   官方微博 | 高级检索  
     检索      

提高无陀螺捷联惯导系统角速度解算精度的新方法
引用本文:赵龙,陈哲.提高无陀螺捷联惯导系统角速度解算精度的新方法[J].系统仿真学报,2003,15(4):579-580,603.
作者姓名:赵龙  陈哲
作者单位:北京航空航天大学自动化科学与电气工程学院,北京,100083
基金项目:航天科技创新基金,北航基础性研究博士生培养基金项目资助
摘    要:在无陀螺捷联惯导系统中,由于合弃陀螺而使系统具有很多优点,但角速度需从加速度计输出的信号中解算出来,且它的解算误差随时间而发散。所以,抑制角速度解算误差的发散,提高其解算精度是该项技术研发的关键。提出了一种在九加速度方案下提高角速度解算精度的新方法,它是一种利用冗余信息得到残余误差方程,再进行数值迭代的方法。该方法比建立噪声状态估计、利用卡尔曼滤波束修正姿态的方法简单而有效。仿真结果表明,利用此方法能明显提高系统角速度解算精度。

关 键 词:无陀螺捷联惯导系统  角速度解算精度法  冗余信息  仿真
文章编号:1004-731X(2003)04-0579-02

A New Method for Improving the Angular Velocity Calculation Precision of Gyroscope-Free Strapdown Inertial Navigation System
ZHAO Long,CHEN Zhe.A New Method for Improving the Angular Velocity Calculation Precision of Gyroscope-Free Strapdown Inertial Navigation System[J].Journal of System Simulation,2003,15(4):579-580,603.
Authors:ZHAO Long  CHEN Zhe
Abstract:There are many strengths in the gyroscope-free strapdown inertial navigation system because it is gyroscopes- free; the angular velocity, however, is calculated from signals that are sent by accelerometers, and its calculation error is divergent in time. The key technique, therefore, is how to control the divergence of the angular velocity calculation error and improve the calculation precision. To do the latter in nine-accelerometers schemes, a new method is provided, in which the equation of residual errors is firstly obtained by using the redundant information, then the numerical iteration is applied. The method is simpler and more effective than that one, which uses Kalman filtering to correct satellite attitude errors in the real time after a state noise estimation is received. Simulation results show that the angular velocity calculation precision is obviously improved by the new method.
Keywords:gyroscope-free strapdown inertial navigation system  redundant information  accelerometers  angular velocity calculation precision  estimation algorithm
本文献已被 CNKI 维普 万方数据 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号