Stability Tracking Control Methods and Applications of the Missile Launching Equipment Under the Coupling of the Wheeled Vehicle

JIANG Xiaoming; LIU Yigang; NIU Yuanzheng; YIN Xiang

doi:10.15892/j.cnki.djzdxb.2023.06.015

Journal of Projectiles, Rockets, Missiles and Guidance >

2023 , Vol. 43 >Issue 6: 92 - 96

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2023.06.015

Stability Tracking Control Methods and Applications of the Missile Launching Equipment Under the Coupling of the Wheeled Vehicle

JIANG Xiaoming ,
LIU Yigang ,
NIU Yuanzheng ,
YIN Xiang

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Shanghai Electro-mechanical Engineering Institute, Shanghai 201109, China

Received date: 2023-07-25

Online published: 2024-12-30

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Abstract

Considering the impact of vehicle flexibility on stability of the missile launching equipment, the rigid-flexible coupling model between the missile launching equipment and wheeled vehicle is proposed in the geographical coordinate system. Then the impact of vehicle flexibility on stability of the servo system of the missile launching equipment is analyzed, and stability conditions of the servo system under the coupling of vehicle and launcher are proposed. The tracking filter in the stabilization control loop is designed to filter the attitude angle of the vehicle for avoiding the instability of the control system under the coupling. Finally the effectiveness of the proposed method is validated by the simulation and experiment.

Key words： wheeled vehicle; missile launching equipment; resonance characteristics; tracking stability

Cite this article

JIANG Xiaoming , LIU Yigang , NIU Yuanzheng , YIN Xiang . Stability Tracking Control Methods and Applications of the Missile Launching Equipment Under the Coupling of the Wheeled Vehicle[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2023 , 43(6) : 92 -96 . DOI: 10.15892/j.cnki.djzdxb.2023.06.015

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References

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[1]	宁变芳, 刘欢, 薛庆阳, 等. 悬挂特性对某高炮射击密集度的影响研究[J]. 火炮发射与控制学报, 2020, 41(4): 12-16. NING B F, LIU H, XUE Q Y, et al. A study of the influence of suspension characteristics on the firing intensity of an anti-aircraft gun[J]. Journal of Gun Launch & Control, 2020, 41(4): 12-16.

[2]	罗中峰, 管小荣, 徐诚. 某自行火炮底盘与火力系统匹配研究[J]. 火力与指挥控制, 2019, 44(6): 41-47. LUO Z F, GUAN X R, XU C. Study on the match between the chassis and the fire system of a self-propelled gun[J]. Fire Control & Command Control, 2019, 44(6): 41-47.

[3]	徐伟国, 毕世华. 导弹发射车悬架的多目标集成优化[J]. 弹箭与制导学报, 2009, 29(2): 246-250. XU W G, BI S H. Multi-objective integrated optimization of the missile transporter-launcher suspensions[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2009, 29(2): 246-250.

[4]	徐伟国, 毕世华, 陈阵. 导弹发射车主动控制悬架多工况减振研究[J]. 兵工学报, 2007, 28(8): 909-914. XU W G, BI S H, CHEN Z. Research on vibration damping for missile launcher with active suspensions under multiple-loading case[J]. Acta Armamentarii, 2007, 28(8): 909-914.

[5]	曾伟, 姜毅. 导弹发射车悬架半主动控制与仿真[J]. 现代防御技术, 2015, 43(1): 146-150. ZENG W, JIANG Y. Semi-active control and simulation of suspension system for launch vehicle[J]. Modern Defence Technology, 2015, 43(1): 146-150.

[6]	麻小明, 刘馨心, 李正宇, 等. 某车载防空系统行进间发射动力学仿真分析与研究[J]. 弹箭与制导学报, 2019, 39(1): 151-154. MA X M, LIU X X, LI Z Y, et al. Dynamic simulation analysis and research of the vehicle-mounted air defense system launching on the move[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2019, 39(1): 151-154.

[7]	杜振宇, 王学智, 程永强. 车载导弹刚柔耦合系统发射过程仿真分析[J]. 弹箭与制导学报, 2017, 37(1): 15-18. DU Z Y, WANG X Z, CHENG Y Q. Simulation analysis of launching process of vehicular missile's rigid-flexible coupling system[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2017, 37(1): 15-18.

[8]	刘伟鹏, 袁杰波, 秦峰, 等. 地空导弹垂直发射高精度初始姿态获取技术研究[J]. 空天防御, 2018, 1(4): 24-28. LIU W P, YUAN J B, QIN F, et al. Study on obtainment of high accuracy initial attitude for vertical launching of ground-to-air missile[J]. Air & Space Defense, 2018, 1(4): 24-28.

[9]	陈余军, 姜毅. 车载导弹行进间发射动力学仿真分析[J]. 弹箭与制导学报, 2011, 31(1): 55-58. CHEN Y J, JIANG Y. Dynamic simulation analysis of mobile missile launching on the move[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2011, 31(1): 55-58.

[10]	赵君伟, 张家骏, 张程, 等. 基于ADAMS与AMESim的飞行器发射动力学仿真[J]. 弹箭与制导学报, 2021, 41(5): 46-52. ZHAO J W, ZHANG J J, ZHANG C, et al. Simulation of launch dynamics of aircraft based on ADAMS and AMESim[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2021, 41(5): 46-52.

[11]	刘馨心, 袁野, 周昌盛, 等. 某大型制导火箭弹发射动力学仿真与试验分析[J]. 弹箭与制导学报, 2020, 40(5): 118-121. LIU X X, YUAN Y, ZHOU C S, et al. Launching dynamics simulation and test analysis of a large guided rocket[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2020, 40(5): 118-121.

[12]	赵修平, 王天辉, 林琨山, 等. 导弹发射装置伺服系统模糊PID控制研究[J]. 现代防御技术, 2012, 40(3): 63-66. ZHAO X P, WANG T H, LIN K S, et al. Missile launcher's servo system based on fuzzy PID controller[J]. Modern Defence Technology, 2012, 40(3): 63-66.

[13]	王康, 林子瑛, 程伟民, 等. 重载发射装置俯仰伺服系统自适应鲁棒控制[J]. 战术导弹技术, 2020 (3): 49-58. WANG K, LIN Z Y, CHENG W M, et al. Adaptive robust control for the pitch servo system of heavy load launcher[J]. Tactical Missile Technology, 2020(3): 49-58.

[14]	王超, 汪国胜, 李睿, 等. 坦克装甲车辆主动悬挂结构技术发展综述[J]. 兵工学报, 2020, 41(12): 2579-2592. WANG C, WANG G S, LI R, et al. Review of state of the art of active suspension structure technology of tank and armored vehicle[J]. Acta Armamentarii, 2020, 41(12): 2579-2592. DOI

[15]	朱鑫, 刘晓昂, 陈勇, 等. 纯电动汽车动力总成悬置系统设计方法[J]. 噪声与振动控制, 2019, 39(2): 85-89. DOI ZHU X, LIU X A, CHEN Y, et al. Design method of the powertrain mounting system of pure electric vehicles[J]. Noise and Vibration Control, 2019, 39(2): 85-89.

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