Resonance Mechanism and Aerodynamic Optimization of a Canard-Type Two-Dimensional Trajectory Correction Projectile in the Uncontrolled Flight Phase

GUO Han; PENG Zhiling; LIU Wenan; LI Guangcai; TAO Ruiping

doi:10.12382/bgxb.2026.0534

您当前的位置：

首页 >

文章列表页 >

Resonance Mechanism and Aerodynamic Optimization of a Canard-Type Two-Dimensional Trajectory Correction Projectile in the Uncontrolled Flight Phase

更新时间：2026-08-21

- Resonance Mechanism and Aerodynamic Optimization of a Canard-Type Two-Dimensional Trajectory Correction Projectile in the Uncontrolled Flight Phase
- Acta Armamentarii (2026)
- 作者机构：
  
  1. 中北大学机电工程学院,山西,太原,030051
  2. 中国兵器工业集团淮海工业集团有限公司,山西,长治,046012
- 作者简介：
- 基金信息：
- DOI：10.12382/bgxb.2026.0534
  CLC： TJ011.3
- Received：16 June 2026，
  
  Online First：21 August 2026，
- 稿件说明：
移动端阅览
郭含，彭志凌，柳文安，等. 鸭舵式二维修正弹无控段共振机理研究及气动优化[J/OL]. 兵工学报, 2026(2026-08-21). https://doi.org/10.12382/bgxb.2026.0534.

GUO H, PENG Z L, LIU W A, et al. Resonance mechanism and aerodynamic optimization of a canard-type two-dimensional trajectory correction projectile in the uncontrolled flight phase[J/OL]. Acta Armamentarii, 2026(2026-08-21). https://doi.org/10.12382/bgxb.2026.0534. (in Chinese)
郭含，彭志凌，柳文安，等. 鸭舵式二维修正弹无控段共振机理研究及气动优化[J/OL]. 兵工学报, 2026(2026-08-21). https://doi.org/10.12382/bgxb.2026.0534. DOI：

GUO H, PENG Z L, LIU W A, et al. Resonance mechanism and aerodynamic optimization of a canard-type two-dimensional trajectory correction projectile in the uncontrolled flight phase[J/OL]. Acta Armamentarii, 2026(2026-08-21). https://doi.org/10.12382/bgxb.2026.0534. (in Chinese) DOI：

摘要

针对鸭式二维修正双旋弹无控段速度与加速度周期性波动问题，从刚体角运动与非线性气动力学出发研究其共振机理与外形优化方法。利用复攻角理论揭示了鸭舵扰动与弹体固有频率共振引发弹道波动的机理，在转速与速度刚性约束下，提出减小舵翼翼展、增大舵偏角调控方案，并基于CFD方法对5种典型外形开展仿真对比。结果表明：缩减翼展可提高俯仰力矩导数，抬升弹体固有频率以规避共振；合理增大舵偏角可匹配操纵力矩变化，使力矩处于适宜范围。该方案有效抑制了弹道参数波动，整体气动特性良好，可在保障修正功能的同时提升飞行稳定性。

Abstract

Aiming at periodic fluctuation of velocity and acceleration for canard-configured two-dimensional correction dual-spin projectiles in uncontrolled flight phase

the resonance mechanism and shape optimization method were studied based on rigid-body angular motion and nonlinear aerodynamics. Complex angle of attack theory revealed how canard disturbance resonates with projectile natural frequency and causes ballistic fluctuation. A canardspanreduction and deflection angle increase scheme was proposed under fixed flight speed and spin rate constraints. Computational Fluid Dynamics (CFD) simulations compared five typical projectile shapes. The results showed that reduced canard span raises pitching moment derivative and projectile natural frequency to avoid resonance

and properly increased deflection angle optimizes control moment. This scheme restrains ballistic fluctuation

maintains good aerodynamic performance

improves flight stability while ensuring correction capability

and provides

关键词

Keywords

references

邢炳楠,杜忠华,杜成鑫.二维弹道修正弹及其制导控制技术综述[J].国防科技大学学报,2021,43(4):53-68.

Xing B N, Du Z H, Du C X. Review on two-dimensional trajectory correction projectile and its guidance and control technology[J]. Journal of National University of Defense Technology, 2021, 43(4):53-68.(in Chinese)

NORRIS J, HAMEED A, ECONOMOU J, et al. A review of dual-spin projectile stability[J]. Defence Technology, 2020, 16(1):1-9.

PHILIPPE W, SPILIOS T. Modelling and stability analysis for a class of 155 mm spin-stabilized projectiles with course correction fuse (CCF)[C]//AIAA atmospheric flight mechanics conference 2011, USA: American Institute of Aeronautics and Astronautics, 2011:223-236.

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)

李红云,申强,邓子龙. 鸭式布局二维修正双旋弹角运动及转向响应特性分析[J].兵工学报,2024, 45 (6):1866-1876.

LI H Y, SHEN Q, DENG Z L. Analysis of angular motion and swerving response characteristics of dual⁃spinning two⁃dimensional correction projectile with canard layout[J]. Acta Armamentarii, 2024, 45(6):1866-1876.(in Chinese)

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)

张衍儒,肖练刚,邱奕,等. 双旋静稳定弹的共振不稳定研究[J].航天控制,2016,34(3):31-35.

ZHANG Y R, XIAO L G, QIU Y, et al. Research on resonance instability of dual-spin static stability projectile[J]. Aerospace Control, 2016, 34(3):31-35. (in Chinese)

柯知非,高敏,王毅,等. 基于二维修正组件的弹道修正弹稳定性分析与仿真研究[J].火炮发射与控制学报,2019,40(2):26-32.

KE Z F, GAO M, WANG Y, et al. Stability analysis and simulation of the trajectory correction projectile based on 2-D correction fuze[J]. Journal of Gun Launch& Control, 2019, 40(2):26-32.(in Chinese)

王钰,于纪言,王晓鸣,等.修正组件结构参数对旋转稳定弹道修正弹稳定性的影响研究[J].兵工学报,2018,39(10):1910-1918.

WANG Y, YU J Y, WANG X M, et al. The influence of correction fuze’s structure parameters on the stability of spin-stabilized projectile[J]. Acta Armamentarii, 2018, 39(10):1910-1918.(in Chinese)

王小康,申强,王晗瑜,等.双旋弹道修正引信的惯导外杆臂误差分析与补偿[J].兵工学报,2025,46(6):34-42.

WANG X K, SHEN Q, WANG H Y, et al. Analysis and compensation of inertial navigation external gimbal arm error for the fuze of double spin ballistic correction projectile[J]. Acta Armamentarii, 2025, 46(6):34-42.(in Chinese)

Luo X, Zhang M, Deng Z, et al. Integrated optimization of de-spin actuator design and operating parameters for tail-controlled flight vehicle[J]. Aerospace Science and Technology, 2025, 167110625-110625.

李红云,申强,邓子龙,等.鸭式布局二维修正旋转稳定弹受控角运动响应特性研究[J].兵工学报,2026,47(2):151-163.

LI H Y, SHEN Q, DENG Z L, et al. The response characteristics of controlled angular motion of the two-dimensional correction spin-stabilized projectile with canard configuration[J]. Acta Armamentarii, 2026, 47(2):151-163.(in Chinese)

史凯,张倩,刘马宝. 155 mm固定翼双旋弹二维弹道修正引信的翼面转速特性及修正能力研究[J].兵工学报,2019,40(8):1587-1595.

SHI K, ZHANG Q, LIU M B. Analysis of spin rate and correction ability of two-dimensional trajectory correction fuze for 155 mm fixed-canard dual-spin projectiles[J]. Acta Armamentarii, 2019, 40(8):1587-1595.(in Chinese)

杨宝清,杨东晓,朱远海.迫击炮可动舵二维修正引信气动特性研究[J].兵器装备工程学报,2020,41(2):30-34.

YANG B Q, YANG D X, ZHU Y H. Study on Aerodynamic characteristics of two-dimensional modified fuze for movable rudder of mortar[J]. Journal of Ordnance Equipment Engineering, 2020, 41(2):30-34.(in Chinese)

KRISHNA A B, KOTHARI M, ABHISHEK A. Guidance and control of spin⁃stabilized projectiles based on super twisting algorithm [J]. Journal of Guidance, Control, and Dynamics, 2022,46(5):1-17.

申强,仇李良,蒲文洋,等.高旋弹二维修正引信双旋结构气动特性及气动力表征[J].北京理工大学学报,2024,44(4):359-368.

SHEN Q, CHOU L L, PU W X, et al. Aerodynamic characteristics and characterization of the double spin structure of two-dimensional correction high-spin projectile[J]. Journal of Beijing Institute of Technology, 2024, 44(4):359-368.(in Chinese)

JAISWAL R, KOTHARI M, ABHISHEK A. Design and aerodynamic characterization of canard guided fuze for dual-spin artillery projectiles[C]//Propeller-rotorcraft-wind Turbine Aerodynamics, vol. 4. 2024: 2176-2186.

RAMTEKE V, KOTHARI M. Accessibility analysis and robust control design of dual-spin projectiles[J]. Journal of Guidance, Control, and Dynamics, 2025,48(3): 575-590.

黄成,王中原,常思江.旋转稳定弹动力学弹道特性分析[J].北京理工大学学报,2024,44(9):904-912.

HUANG C, WANG Z Y, CHANG S J. Dynamic ballistic characteristics of spin-stabilized projectiles[J]. Journal of Beijing Institute of Technology, 2024, 44(9):904-912.(in Chinese)

赵新新,史金光,王中原,等.固定鸭舵双旋弹全弹道动态稳定性及其影响因素[J].力学学报,2022,54(5):1364-1374.

ZHAO X X, SHI J G, WANG Z Y, et al. Dynamic stability and influence factors of the whole trajectory of fixed canard dual⁃spin projectiles[J]. Chinese Journal of Theoretical and Applied Mechanics, 2022, 54(5):1366-1376.(in Chinese)

商霖,张海瑞,孙向春,等.火箭横向模态耦合型自激振动的稳定性分析与仿真模拟[J].国防科技大学学报,2025,47(3):73-80.

SHANG L, ZHANG H R, SUN X C, et al. Stability analysis and simulation of transverse mode-coupled self-excited vibration of rocket [J] Journal of National University of Defense Technology, 2025, 47(3):73-80.

王钰.固定鸭舵式二维弹道修正炮弹控制规律和修正策略研究[D].南京:南京理工大学,2019:22.

WANG Y. Analysis of guidance and corrective strategy for a spin-stabilized projectile equipped with fixed canards[D], Nanjing: Nanjing University of Science&Technology,2019:22. (in Chinese)

朱少雄,施冬梅,王毅.固定舵二维弹道修正弹气动特性分析[J].战术导弹技术,2017,(2):41-46.

ZHU S X, SHI D M, WANG Y. Aerodynamic characteristics of two-dimensional trajectory correction shell with fixed-wing[J]. Tactical Missile Technology, 2017, (2):41-46.(in Chinese)

朱晓辉,俞梅.基于光纤光栅的等截面悬臂梁固有频率研究[J].半导体光电,2018,39(3):394-397.

ZHU X Y, YU M. Study on natural frequencies of cantilever beam based on fiber grating[J]. Semiconductor Optoelectronics, 2018, 39(3):394-397.(in Chinese)

Views

下载量

CNKI被引量

Alert me when the article has been cited

提交

Tools

Publicity Resources

High-precision 3D Inspection Method Based on Dual-scanning Line Structured Light for Key Engine Components

Research on Actuator Fault-tolerant Control Technology Based on a Unified Dynamic Model

Microstructure Evolution of Pure Copper during Additive Friction Stir Deposition

Analysis of Macroscopically Continuous-microscopic Heterostructured Vehicle Body Structure

Laser Powder Bed Fusion of Aermet100 Steel: Novel Microstructure and Excellent Strength-ductility Combination

Related Author

No data

Related Institution

No data

Postal code：100089
Tel：010-68963060/68962718 Fax：010-68963025 Email：bgxb@cos.org.cn
Technical support is provided by Beijing Founder electronics co., LTD 京ICP备05059581号-4 京公网安备11010802024360号
It is recommended to read the content of this site in Chrome&IE9+. Please switch to extreme mode in browser 360.
Cookies We use cookies to help provide and enhance our service and tailor content. By continuing, you agree to the use of cookies.
Total Visits：256426 Visits Today：844

⁰