周期平均控制下固定翼双旋弹角运动特性分析

doi:10.7527/S1000-6893.2018.22452

电子电气工程与控制

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周期平均控制下固定翼双旋弹角运动特性分析

张鑫¹, 姚晓先¹, 杨忠², 郭致远¹

1. 北京理工大学宇航学院, 北京 100081;
2. 鲁东大学交通学院, 烟台 264025

收稿日期:2018-06-04 修回日期:2018-11-12 出版日期:2019-04-15 发布日期:2018-12-11
通讯作者: 张鑫 E-mail:zxump45@163.com
基金资助:
山东省自然科学基金（ZR2017PEE016）

Analysis of angular motion of dual-spin projectile with fixed-canards under period average control

ZHANG Xin¹, YAO Xiaoxian¹, YANG Zhong², GUO Zhiyuan¹

1. School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China;
2. College of Transportation, Ludong University, Yantai 264025, China

Received:2018-06-04 Revised:2018-11-12 Online:2019-04-15 Published:2018-12-11
Supported by:
Shandong Provincial Natural Science Foundation of China (ZR2017PEE016)

摘要/Abstract

摘要： 针对应用在固定翼双旋弹上的一种周期平均控制方法，通过对弹体修正组件滚转角进行傅里叶变换，得到了双旋弹在周期平均控制下角运动方程的模型，进而分析了周期平均控制下固定翼双旋弹的角运动响应，并根据双旋弹角运动特性和执行机构的性能限制给出了周期平均控制角频率的设计方法。引进2种具体的周期平均控制方案作为分析对象，并通过六自由度弹道仿真进行了验证。结果表明，对固定翼双旋弹角运动响应的分析能够反映周期平均控制的特性，周期平均控制角频率的设计方法可以设计出合理的角频率。

关键词: 固定翼, 双旋弹, 周期平均, 角运动, 角频率

Abstract: To study the period average control method applied to the dual-spin projectile with fixed-canards, the Fourier transform of the roll angle of the course correction fuse is used to obtain the angular motion model for the dual-spin projectile under period average control. Then the angular motion of the dual-spin projectile with fixed-canards under period average control is analyzed. A design of the angular frequency of the period average control is proposed based on the performance of the angular motion and the performance limitations of the actuator. Two specific designs are analyzed and verified through six degrees of freedom simulations. The results indicate that the analyses of the angular motion of the dual-spin projectile with fixed-canards can reveal the properties of the period average control method, and the designed method can produce proper angular frequencies.

Key words: fixed-canard, dual-spin projectile, period average, angular motion, angular frequency

中图分类号:

V212
TJ765.1

张鑫, 姚晓先, 杨忠, 郭致远. 周期平均控制下固定翼双旋弹角运动特性分析[J]. 航空学报, 2019, 40(4): 322452-322452.

ZHANG Xin, YAO Xiaoxian, YANG Zhong, GUO Zhiyuan. Analysis of angular motion of dual-spin projectile with fixed-canards under period average control[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(4): 322452-322452.

参考文献

[1] REGAN F J, SMITH J. Aeroballistics of a terminally corrected spinning projectile (TCSP)[J]. Journal of Spacecraft and Rockets, 1975, 12(12):733-738.
[2] HAMEL N, GAGNON E. CFD and parametric study on a 155 mm artillery shell equipped with a roll-decoupled course correction fuze[C]//29th AIAA Applied Aerodynamics Conference. Reston, VA:AIAA, 2011:1-10.
[3] 曹红锦. 美国精确制导组件技术发展现状分析[J]. 四川兵工学报, 2015, 36(9):22-25. CAO H J. Analysis of the development status of American precision guidance kit technology[J]. Journal of Sichuan Ordnance, 2015, 36(9):22-25(in Chinese).
[4] COSTELLO M, PETERSON A. Linear theory of a dual-spin projectile in atmospheric flight[J]. Journal of Guidance, Control, and Dynamics, 2000, 23(5):789-797.
[5] WERNERT P, LEOPOLD F, LEHMANN L, et al. Wind tunnel tests and open-loop trajectory simulations for a 155 mm canards guided spin stabilized projectile[C]//AIAA Atmospheric Flight Mechanics Conference and Exhibit. Reston, VA:AIAA, 2008:1-17.
[6] WERNERT P. Stability analysis for canard guided dual-spin stabilized projectiles[C]//AIAA Atmospheric Flight Mechanics Conference and Exhibit. Reston, VA:AIAA, 2009:1-24.
[7] WERNERT P, THEODOULIS S. Modelling and stability analysis for a class of 155 mm spin-stabilized projectiles with course correction fuse (CCF)[C]//AIAA Atmospheric Flight Mechanics Conference and Exhibit. Reston, VA:AIAA, 2011:1-14.
[8] THEODOULIS S, WERNERT P. Flight control for a class of 155 mm spin-stabilized projectiles with course correction fuse (CCF)[C]//AIAA Guidance, Navigation, and Control Conference. Reston, VA:AIAA, 2011:1-11.
[9] THEODOULIS S, GASSMANN V, WERNERT P. Guidance and control design for a class of spin-stabilized fin-controlled projectiles[J]. Journal of Guidance, Control, and Dynamics, 2013, 36(2):517-531.
[10] THEODOULIS S, SEVE F, WERNERT P. Robust gain-scheduled autopilot design for spin-stabilized projectiles with a course-correction fuze[J]. Aerospace Science and Technology, 2015, 42:477-489.
[11] SEVE F, THEODOULIS S, WERNERT P, et al. Flight dynamics modeling of dual-spin guided projectiles[J]. IEEE Transactions on Aerospace and Electronic Systems, 2017, 53(4):1625-1641.
[12] CHANG S J, WANG Z Y, LIU T Z. Analysis of spin-rate property for dual-spin-stabilized projectiles with canards[J]. Journal of Spacecraft and Rockets, 2014, 51(3):958-966.
[13] 许诺, 于剑桥, 王亚飞, 等. 固定翼双旋弹动力学特性分析[J]. 兵工学报, 2015, 36(4):602-609. XU N, YU J Q, WANG Y F, et al. Analysis of dynamic characteristics of fixed-wing dual-spin projectiles[J]. Acta Armamentarii, 2015, 36(4):602-609(in Chinese).
[14] 许诺, 于剑桥, 王亚飞. 固定翼双旋弹动力学分岔特性分析[J]. 航空学报, 2015, 36(12):3798-3808. XU N, YU J Q, WANG Y F. Dynamic bifurcation characteristics analysis on fixed-canard dual-spin projectiles[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(12):3798-3808(in Chinese).
[15] 常思江, 王中原, 刘铁铮. 鸭式布局双旋稳定弹强迫运动理论研究[J]. 兵工学报, 2016, 37(5):829-839. CHANG S J, WANG Z Y, LIU T Z. A theoretical study of forced motion for dual-spin-stabilized projectiles with canards[J]. Acta Armamentarii, 2016, 37(5):829-839(in Chinese).
[16] 张冬旭. 可控滚转二维弹道修正机构的研究[D]. 北京:北京理工大学, 2015:19-39. ZHANG D X. Research on the rolling controlled two-dimensional trajectory correction mechanism[D]. Beijing:Beijing Institute of Technology, 2015:19-39(in Chinese).
[17] 许诺, 于剑桥, 王亚飞. 基于周期平均的固定翼双旋弹弹道修正方法[J]. 航空学报, 2015, 36(9):2892-2899. XU N, YU J Q, WANG Y F. Trajectory correcting method of fixed-canard dual-spin projectiles based on period average[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(9):2892-2899(in Chinese).
[18] 郭致远, 姚晓先, 张鑫. 基于周期平均的固定舵双旋火箭弹控制方法[J]. 航空学报, 2017, 38(12):321307. GUO Z Y, YAO X X, ZHANG X. Control method for a class of fixed-canard dual-spin rockets based on period average[J]. Acta Aeronautica et Astronautica Sinica, 2017, 38(12):321307(in Chinese).
[19] 韩子鹏. 弹箭外弹道学[M]. 北京:北京理工大学出版社, 2008:127-149. HAN Z P. Exterior ballistics of projectiles and rockets[M]. Beijing:Beijing Institute of Technology Press, 2008:127-149(in Chinese).
[20] 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, 2008:53-55. QIAN X F, LIN R X, ZHAO Y N. Missile flight mechanics[M]. Beijing:Beijing Institute of Technology Press, 2008:53-55(in Chinese).

E-mail：hkxb@buaa.edu.cn

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主管单位：中国科学技术协会主办单位：中国航空学会北京航空航天大学

周期平均控制下固定翼双旋弹角运动特性分析

Analysis of angular motion of dual-spin projectile with fixed-canards under period average control

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