中国惯性技术学报
中國慣性技術學報
중국관성기술학보
JOURNAL OF CHINESE INERTIAL TECHNOLOGY
2013年
2期
182-185
,共4页
毛玉良%陈家斌%宋春雷%刘朝华
毛玉良%陳傢斌%宋春雷%劉朝華
모옥량%진가빈%송춘뢰%류조화
捷联惯导%四元数%旋转矢量%误差模型
捷聯慣導%四元數%鏇轉矢量%誤差模型
첩련관도%사원수%선전시량%오차모형
SINS%quaternion%rotation vector%error model
捷联惯性导航系统以数字平台代替了平台惯导的机械平台.所谓数字平台,即存储在导航计算机中的坐标变换矩阵.四元数和旋转矢量是用来描述捷联惯导系统姿态的两种常用方法.传统的线性误差模型如 psi 角误差模型、等效倾角误差模型,仅仅适用于误差角非常小的情况.对于误差角比较大的系统,误差模型变得非线性,由此引入旋转矢量误差模型.通过对加性四元数、乘性四元数以及旋转矢量误差模型的分析表明,三者是等价的,并且当误差角很小的时候,乘性四元数误差模型和旋转矢量误差模型可以退化为等效倾角误差模型.
捷聯慣性導航繫統以數字平檯代替瞭平檯慣導的機械平檯.所謂數字平檯,即存儲在導航計算機中的坐標變換矩陣.四元數和鏇轉矢量是用來描述捷聯慣導繫統姿態的兩種常用方法.傳統的線性誤差模型如 psi 角誤差模型、等效傾角誤差模型,僅僅適用于誤差角非常小的情況.對于誤差角比較大的繫統,誤差模型變得非線性,由此引入鏇轉矢量誤差模型.通過對加性四元數、乘性四元數以及鏇轉矢量誤差模型的分析錶明,三者是等價的,併且噹誤差角很小的時候,乘性四元數誤差模型和鏇轉矢量誤差模型可以退化為等效傾角誤差模型.
첩련관성도항계통이수자평태대체료평태관도적궤계평태.소위수자평태,즉존저재도항계산궤중적좌표변환구진.사원수화선전시량시용래묘술첩련관도계통자태적량충상용방법.전통적선성오차모형여 psi 각오차모형、등효경각오차모형,부부괄용우오차각비상소적정황.대우오차각비교대적계통,오차모형변득비선성,유차인입선전시량오차모형.통과대가성사원수、승성사원수이급선전시량오차모형적분석표명,삼자시등개적,병차당오차각흔소적시후,승성사원수오차모형화선전시량오차모형가이퇴화위등효경각오차모형.
In strapdown inertial navigation system(SINS), the digital platform is the coordinate transformation matrix stored in the navigation computer, whose functions are the same as that of mechanical platform in the gimbaled navigation system. The quaternions and the rotation vector are two commom methods to describe the attitude of SINS. The conventional linearized error models, such as psi-angle model and the equivalent tilt (ET) model, are effective only for the systems with infinitesimal attitude errors. In this paper, the rotation vector error(RVE) model was introduced as a nonlinear error model for the systems with large attitude error. The attitude error models in terms of additive quaternion, multiplicative quaternion and rotation vector were presented respectively, and they were found to be equivalent among them. Besides, the multiplicative quaternion error model and the rotation vector error model can be reduced to ET model in case the system’s attitude errors are very small.