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挠性陀螺系统不对称性误差研究
Analysis on non-symmetrical error in dynamically tuned gyro system
【摘要】 首先从原理上分析其产生的原因,不对称性误差主要是由于陀螺系统中各环节的输入-输出关系并不是理想的线性特性而引起的;然后对陀螺系统不对称性误差进行定量分析,采用一种寻优的方法估算出不对称性误差值大小,并用实验进行验证;最后提出了一种不对称性误差的补偿方法,即在陀螺角速度模型中增加角速度绝对值项。实验结果证明了其简单有效性。
【Abstract】 The cause that generated asymmetric error was analyzed from the gyro’s principle and it was found that the main reason was that the output-input relations in dynamically tuned gyro system was not ideally linear.The paper then made a quantitative analysis for the asymmetric error,and applied a finding-minimum-search method to estimate the error’s value and verified by experiment.A compensatory algorithm was proposed which added the absolute angular-rate into the gyro module.The experiment result proved its effectiveness and simplicity.
【关键词】 惯性导航;
不对称性误差;
误差补偿;
寻优方法;
【Key words】 inertial navigation system; asymmetric error; error compensation; finding-minimum-search;
【Key words】 inertial navigation system; asymmetric error; error compensation; finding-minimum-search;
- 【文献出处】 中国惯性技术学报 ,Journal of Chinese Inertial Technology , 编辑部邮箱 ,2006年06期
- 【分类号】U666.123
- 【被引频次】4
- 【下载频次】176