[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 >
Design of the Rotary Measurement and Control System for Double-spinning Projectile
Received date: 2018-03-31
Online published: 2025-05-20
The measurement and control system based on permanent magnet ac generator, which performs functions of executive steering gear and load power, was designed to make accurate trajectory correction for the double-spinning projectile. A calculation model of the rudder's rolling Angle in inertial system was also established. A new method combining software and hardware filtering and compensation was put forward in order to reduce the strong magnetic interference of the steering gear on the geomagnetic sensor. A dual closed-loop control system architecture which combines the incremental PID control strategy was adopted. The generation voltage is in the range of 10 ~ 90.6 V when the steering gear is in the range of 80~500 Hz; The rotational speed measuring precision of the projectile and rudder is better than 0.1 Hz, and the rudder position measuring precision is better than 1°. Shooting range experiment results prove that the system response time of speed control is better than 0.1 s, and the stability of position control is better than 5°. Conclusions show that the steering gear system has good feasibility and reliability underground and missile-borne conditions.
LI Hao , JIA Fangxiu , YU Jiyan , ZHOU Qiang , ZHANG Tianyu . Design of the Rotary Measurement and Control System for Double-spinning Projectile[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2019 , 39(2) : 69 -74 . DOI: 10.15892/j.cnki.djzdxb.2019.02.017
| [1] | REGAN F J, SMITH J. Aeroballistics of a terminally corrected spinning projectile (TCSP)[J]. Journal of Spacecraft & Rockets, 1975. 12 (12): 733- 738. |
| [2] | CHENG J, WANG X M, YU JY, et al. On the response of spin stabilized projectile to side force by angular motion and impact[C]// Proceedings of 27th International Symposium on Ballistics. Orlando: IBS, 2013: 78- 96. |
| [3] | BYBEE T. Precision guidance kit C// Proceedings of 45th Annual NDIA Gun and Missile Systems Conference. Dallas: NDIA, 2010: 1- 12. |
| [4] | 郑斌, 王磊, 沈卫, et al. 世界兵器发展年度报告[R]. 北京: 中国兵器工业集团第210研究所, 2012. |
| [5] | 高峰, 张合. 基于地磁探测和脉冲力控制的二维弹道修正系统仿真[J]. 学报, 2011, 23 (1): 123- 128. |
| [6] | 陈胜政, 杨波, 杨栓虎, et al. 脉冲修正弹药技术研究[J]. 兵器装备工程学报, 2017, 38 (12): 60- 64. |
| [7] | YANG Shuxing, YAN Xiaoyong, XIONG Fenfen. Trend of the artillery rocket and the problems related to control[C]// CHEN Jie. Proceedings of the 29th Chinese Control Conference. Beijing: Beihang University Press, 2010: 6– 13. |
| [8] | 纪秀玲, 王海鹏, 曾时明, et al. 可旋转鸭舵对旋转弹丸纵向气动特性的影响[J]. 北京理工大学学报, 2011, 31 (3): 265- 268. |
| [9] | 王飞. 基于DSP的反旋舵机控制系统设计[D]. 南京: 南京理工大学, 2013. |
| [10] | 程建伟, 于志远, 姚晓先, et al. 可控滚转舵系统滚转控制研究[J]. 北京理工大学学报, 2010, 30 (6): 670- 673. |
| [11] | 黄建勋. 弹道修正弹电磁式舵机系统设计[D]. 南京: 南京理工大学, 2009. |
| [12] | 骆光照. 电动舵机的鲁棒控制研究[D]. 西安: 西北工业大学, 2003. |
| [13] | 王俊杰. 面向导弹舵机的永磁同步电机及控制方法研究[D]. 哈尔滨: 哈尔滨工业大学, 2013. |
| [14] | 赵国平, 吴红星, 张立华, et al. 永磁同步直线电机直接驱动控制技术[J]. 微电机, 2013, 46 (8): 72- 78. |
| [15] | 曹鹏, 于纪言, 王晓鸣, et al. 基于地磁与卫星组合的高旋弹丸滚转角高频测量及系统误差计算研究[J]. 兵工学报, 2014, 35 (6): 795- 800. |
/
| 〈 |
|
〉 |