[an error occurred while processing this directive] [an error occurred while processing this directive]
[an error occurred while processing this directive]Journal of Projectiles, Rockets, Missiles and Guidance >
Guided Projectile Roll Angle Identification Algorithm based on Rotation Modulation Method
Received date: 2024-09-27
Online published: 2026-01-24
Hypervelocity guided projectiles are survived the high-g loads within the initial launch and required in-flight alignment after power on,the measurement accuracy of MEMS IMU will decrease after high-g load shocks.In order to solve the problem of low accuracy of in-flight alignment,on the premise of not increasing extra mechanism on the projectile,the idea of rotational modulation is presented to realize the self-compensation of MEMS IMU.The method of improving the accuracy of in-flight alignment through the rotation of the projectile itself in the air is proposed.The roll angle identification algorithm based on the rotational modulation method is derived under the single-axis (roll axis) rotation of the projectile.Based on the established ballistic model,the Monte Carlo simulations are carried out using trajectories with different roll angles,different launching azimuths.The simulation results show that the accuracy of roll angle identification is within 3°.Compared with the traditional roll angle identification method,the accuracy of the rotation modulation method is demonstrated.
CHEN Kai , HUANG Peng , JIAO Yong , ZENG Chengzhi , LI Zhenhao , YANG Tao . Guided Projectile Roll Angle Identification Algorithm based on Rotation Modulation Method[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2025 , 45(6) : 1044 -1050 . DOI: 10.15892/j.cnki.djzdxb.2025.06.011
| [1] |
鲁军勇, 冯军红, 李开, 等. 超高速制导弹丸研究综述[J]. 哈尔滨工程大学学报, 2021, 42(10):1418-1427.
|
| [2] |
陈胜政, 杨波, 宋宇航, 等. 制导炮弹姿态测量技术综述[J]. 探测与控制学报, 2021, 43(04):9-13.
|
| [3] |
李小燕, 李杰, 冯凯强, 等. 制导炮弹用INS/GPS组合导航系统空中对准方法[J]. 测试技术学报, 2019, 33(04):329-333.
|
| [4] |
|
| [5] |
|
| [6] |
|
| [7] |
|
| [8] |
贾勇, 秦永元, 李岁劳, 等. 用于短时定位的MEMS旋转调制惯性导航系统[J]. 传感技术学报, 2018, 31(06):963-968.
|
| [9] |
王思远, 罗世彬. 旋转式MEMS惯性导航系统的发展及应用[J]. 传感器与微系统, 2021, 40(06):5-7.
|
| [10] |
罗星航, 刘峰, 刘辉, 等. 基于速度积分匹配的旋转调制惯导系统动基座对准方法[J]. 导航定位与授时, 2021, 8(05):32-37.
|
| [11] |
莫明岗. 旋转制导炮弹用惯性导航系统空中对准方法研究[D]. 哈尔滨工业大学, 2020.
|
| [12] |
孙伟. 旋转调制型捷联惯性导航系统[M]. 北京: 测绘出版社, 2014.
|
| [13] |
|
| [14] |
陈凯, 张通, 刘尚波. 捷联惯导与组合导航原理[M]. 西安: 西北工业大学出版社, 2021.
|
| [15] |
|
/
| 〈 |
|
〉 |