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基于地磁传感器的旋转弹箭滚转角解算精度分析

  • 陈胜政 ,
  • 杨波 ,
  • 张意 ,
  • 王天明 ,
  • 杨靖
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  • 西安现代控制技术研究所, 西安 710065

陈胜政(1982-),男,陕西西安人,高级工程师,硕士,研究方向:制导弹药总体设计。

收稿日期: 2019-06-04

  网络出版日期: 2025-02-12

Accuracy Analysis of Rolling Angle of Rotating Projectile Based on Geomagnetic Sensor

  • CHEN Shengzheng ,
  • YANG Bo ,
  • ZHANG Yi ,
  • WANG Tianming ,
  • YANG Jing
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  • Xi’an Modern Control Technology Research Institute, Xi’an 710065, China

Received date: 2019-06-04

  Online published: 2025-02-12

摘要

制导旋转弹箭的命中精度与其滚转角信号的解算精度密切相关。地磁传感器作为一种低成本的滚转角解算手段得到广泛使用。为对其解算精度进行分析,文中建立了误差模型,并进行了仿真分析。结果表明,滚转角精度主要取决于北向角的取值范围。当北向角大于35°时,解算精度较高,有利于保证弹箭射击精度。而当北向角小于15°时,滚转角误差急剧发散,使得弹箭射击精度变差。文中的分析研究可为弹箭控制系统设计及作战使用提供一定的指导。

本文引用格式

陈胜政 , 杨波 , 张意 , 王天明 , 杨靖 . 基于地磁传感器的旋转弹箭滚转角解算精度分析[J]. 弹箭与制导学报, 2020 , 40(3) : 139 -143 . DOI: 10.15892/j.cnki.djzdxb.2020.03.031

Abstract

The hitting accuracy of guided rotating missile is closely related to the accuracy of roll angle signal. Geomagnetic sensors are widely used as a low-cost rolling angle calculation method. In order to analyze the accuracy of its solution, this paper establishes an error model and carries out simulation analysis. The results show that the accuracy of roll angle mainly depends on the range of the northward angle. When the northward angle is more than 35 degrees, the calculation accuracy is higher, which is helpful to ensure the shooting accuracy of projectiles and rockets. When the northward angle is less than 15 degrees, the roll angle error diverges sharply, which makes the shooting accuracy of rockets worse. The analysis and research in this paper can provide some guidance for the design and operation of rocket control system.

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[1]
苟秋雄, 刘明喜, 李虎军. 基于磁阻传感器的末制导迫击炮弹滚转姿态初始对准技术研究[J]. 弹箭与制导学报, 2008, 28(3):45-48.

[2]
KAYASAL Ugur. 磁力计辅助的惯性导航系统:基于IMU和磁力计的导航系统建模和仿真[M]. 卢建华,赵国荣,徐胜红,等译. 北京: 国防工业出版社, 2017:23-27.

[3]
赵敏华, 吴斌, 石萌, 等. 基于GPS与三轴磁强计的联合导航算法[J]. 天文学报, 2006, 47(1):93-99.

[4]
郭才发, 胡正东, 张士峰, 等. 地磁导航综述[J]. 宇航学报, 2009, 30(4):1314-1319.

[5]
马国梁, 李岩, 葛敬飞. 磁阻传感器测量旋转弹滚转姿态的原理分析[J]. 弹道学报, 2012, 24(1):32-36.

[6]
李兴城, 牛宏宇. 基于磁阻传感器的旋转弹姿态测量算法研究[J]. 计算机仿真, 2012, 29(5):51-54.

[7]
鲍亚琪, 陈国光, 吴坤, 等. 基于磁强计和MEMS陀螺的弹箭全姿态探测[J]. 兵工学报, 2008, 29(10):1227-1231.

[8]
KAYASAL Ugur. Magnetometer Aided Inerital Navigation System:Modeling and Simulation of a Navigation System With an IMU and a Magnetometer[M]. Turkey: National Defense Industry Press, 2009:74-77.

[9]
杨荣军, 王良明, 修观, 等. 基于磁强计测量的滚转弹药姿态估计[J]. 海军工程大学学报, 2011, 23(5):108-112.

[10]
钱杏芳, 林瑞雄, 赵亚男. 导弹飞行力学[M]. 北京: 北京理工大学出版社, 2011:128-139.

[11]
史金光, 韩艳, 刘世平, 等. 制导炮弹飞行姿态角的一种组合测量方法[J]. 弹道学报, 2011, 23(3):37-42.

[12]
龙达峰, 刘俊, 张晓明, 等. 地磁导航中磁测姿态解算误差分析[J]. 科学技术与工程, 2015, 15(6):204-209.

[13]
郭庆伟, 李超旺. 应用地磁场的弹体飞行姿态测量方法研究[J]. 装备环境工程, 2012, 9(4):106-109.

[14]
赵捍东, 曹红松, 朱基智, 等. 基于磁强计和陀螺的姿态测量方法[J]. 中北大学学报(自然科学版), 2010, 31(6):631-635.

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