Research on in-light alignment error model based on quaternion and rotation vector

被引:0
|
作者
徐国强 [1 ]
孟秀云 [1 ]
机构
[1] School of Aerospace Engineering,Beijing Institute of Technology
关键词
error model; quaternion; in-flight alignment; rotation vector;
D O I
10.15918/j.jbit1004-0579.2011.03.017
中图分类号
V249.3 [导航];
学科分类号
081105 ;
摘要
Euler angle error model,rotation vector error model(RVE)and quaternion error model(QE)were qualitatively and quantitatively compared and an in-flight alignment filter algorithm was designed.This algorithm used extended Kalman filter(EKF)based on RVE and QE separately avoiding the accuracy problem of the Euler angle model and used Rauch-Tung-Striebel(RTS)smoothing method to refine the accuracy recuperating the coning error for simplified RVE.Simulation results show that RVE and QE are more adapt for nonlinear filter estimation than the Euler angle model.The filter algorithm designed has more advantages in convergence speed,accuracy and stability comparing with the algorithm based on the three models separately.
引用
收藏
页码:331 / 338
页数:8
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