Research on rigid-flexible coupling launch dynamics modeling method for a self-propelled anti-aircraft gun

被引：0
|
作者：
Zhang, Xin [1 ]
Wang, Baobao [1 ]
Zhang, Hui [1 ]
Yu, Cungui [2 ]
机构：
[1] China Shipbldg Ind Corp, Res Inst 716, Lianyungang, Jiangsu, Peoples R China
[2] Nanjing Univ Technol, Coll Mech Engn, Nanjing, Jiangsu, Peoples R China
来源：
2021 8TH INTERNATIONAL FORUM ON ELECTRICAL ENGINEERING AND AUTOMATION, IFEEA | 2021年
关键词：
Dynamic simulation; Large caliber artillery; Finite element method;
D O I：
10.1109/IFEEA54171.2021.00164
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
Taking a self-propelled anti-aircraft gun as the research object, based on the simplified model of the self-propelled anti-aircraft gun, the Newton Euler equation and the finite element method were used to conduct the dynamics analysis, and the rigid-flexible coupling dynamics model of the whole gun was constructed by using the direct stiffness method. Modal mode superposition method was used to decouple the equations and solve the attitude of the vehicle body, and the feasibility of the modeling method and the solution method was verified by the finite element software ABAQUS. In this paper, a rigid-flexible coupling launching dynamic modeling method for self-propelled antiaircraft gun is proposed, which is of great significance for launching dynamic modeling of self-propelled antiaircraft gun.
引用
收藏
页码：787 / 793
页数：7
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    Dai, Yingjie
    [J]. PROCEEDINGS OF THE 2ND INTERNATIONAL CONFERENCE ON ELECTRONICS, NETWORK AND COMPUTER ENGINEERING (ICENCE 2016), 2016, 67 : 533 - 538
  • [2] DYNAMICS AND CONTROL OF A GYROSCOPE-STABILIZED PLATFORM IN A SELF-PROPELLED ANTI-AIRCRAFT SYSTEM
    Koruba, Zbigniew
    Dziopa, Zbigniew
    Krzysztofik, Izabela
    [J]. JOURNAL OF THEORETICAL AND APPLIED MECHANICS, 2010, 48 (01) : 5 - 26
  • [3] Rigid-Flexible Coupling Dynamics Analysis Method for Gun Based on Gauss Constraint
    Shi, Y. D.
    Wang, D. S.
    [J]. 2009 IEEE 16TH INTERNATIONAL CONFERENCE ON INDUSTRIAL ENGINEERING AND ENGINEERING MANAGEMENT, VOLS 1 AND 2, PROCEEDINGS, 2009, : 1836 - 1841
  • [4] Vibration analysis of naval gun by rigid-flexible coupling dynamics
    Shi, Yue-Dong
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    [J]. Dandao Xuebao/Journal of Ballistics, 2010, 22 (01): : 37 - 40
  • [5] Modeling methods of rigid-flexible coupling dynamics
    Hong, Jia-Zhen
    Liu, Zhu-Yong
    [J]. Shanghai Jiaotong Daxue Xuebao/Journal of Shanghai Jiaotong University, 2008, 42 (11): : 1922 - 1926
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  • [7] Modeling and Parameter Revising Method of Rigid-Flexible Coupling Dynamics Model
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    [J]. JOURNAL OF COASTAL RESEARCH, 2015, : 720 - 724
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    Xu, Li
    Mao, Bao-Quan
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    Xu, Zhen-Hui
    [J]. Dandao Xuebao/Journal of Ballistics, 2011, 23 (04): : 84 - 89
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  • [10] Natural Vibration Analysis for Gun Using Rigid-Flexible Coupling Multi-body Modeling Method
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    [J]. MECHATRONICS AND INTELLIGENT MATERIALS III, PTS 1-3, 2013, 706-708 : 1437 - 1442
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