中国惯性技术学报2024,Vol.32Issue(11) :1061-1068.DOI:10.13695/j.cnki.12-1222/o3.2024.11.001

混合式惯性导航系统平台转动控制算法设计

Control algorithm design of platform rotation for hybrid inertial navigation system

魏栋 付强文 李炽融 李四海 陶渊博
中国惯性技术学报2024,Vol.32Issue(11) :1061-1068.DOI:10.13695/j.cnki.12-1222/o3.2024.11.001

混合式惯性导航系统平台转动控制算法设计

Control algorithm design of platform rotation for hybrid inertial navigation system

魏栋 1付强文 1李炽融 1李四海 1陶渊博2
扫码查看

作者信息

  • 1. 西北工业大学 自动化学院,西安 710129
  • 2. 中国兵器工业导航与控制技术研究所,北京 100089
  • 折叠

摘要

混合式惯性导航系统(HINS)通过误差调制可以有效提高惯性导航系统的独立导航精度.传统三框架HINS平台转动控制算法能够控制旋转平台实现相对参考系(地理系或惯性系)稳定,但在此基础上叠加误差调制转动时会出现奇异点,使得旋转平台无法按预定方案旋转.针对出现奇异点的问题,分析了HINS在不同导航模式下旋转平台在转动过程中相应坐标系之间的转换关系,并以控制旋转平台达到指定位置为控制目标,利用四元数进行控制指令解算,设计了一种基于坐标系转换关系的四元数旋转平台转动控制算法.通过相应的仿真及实验进行验证,结果表明:所提算法避免了计算框架指令角位置信息时出现奇异点,使得三框架HINS能够按预定方案旋转.

Abstract

Hybrid inertial navigation system(HINS)can effectively improve the independent navigation accuracy of inertial navigation system by using error modulation.The traditional three-frame HINS platform rotation control algorithm can stabilize the rotational platform relative to the reference frame(geographical system or inertial system).However,singularity will appear when error modulation rotation is superimposed on this basis,which makes the rotational platform unable to rotate in a predetermined way.To solve the problem of singularity,the transforming relation between the corresponding coordinate systems during the rotation of HINS rotational platform under different navigation states is analyzed.Taking the control of the rotational platform to reach the specified position as the control goal,the quaternion is used to solve the control instructions,and a quaternion rotational platform control algorithm is designed based on the coordinate transforming relationship.The results of simulation and experiment show that the proposed algorithm avoids singularity when calculating the angular position information of frame instructions,and makes the three-frame HINS rotate in a predetermined way.

关键词

混合式惯性导航系统/平台转动控制/坐标系转换关系/四元数

Key words

hybrid inertial navigation system/platform rotation control/coordinate transforming relation/quaternion

引用本文复制引用

出版年

2024
中国惯性技术学报
中国惯性技术学会

中国惯性技术学报

CSTPCDCSCD北大核心
影响因子:0.792
ISSN:1005-6734
段落导航相关论文