Research on Verification Method of Missile Elastic Suppression Based on Frequency Compensation

doi:10.16182/j.issn1004731x.joss.24-0264

Abstract

Abstract:

For the elastic model of missile body in six degree of freedom mathematical simulation, the research on the verification method of elastic vibration suppression is carried out.. The notch filter used for elastic vibration suppression is introduced, the verification idea for filter design in boost-phase and passive-phase stages of missile flight is analyzed, and the problem currently existing in mathematical simulation verification is pointed out. Based on the frequency modulation phenomenon, an online verification method of frequency compensation for the notch filter is put forward, and it can be found that the function can be applied to any order of elastic frequency verification through the theoretical derivation of the frequency compensation function. The verification of the designed notch filter is achieved by constructing the frequency compensation function of the missile body elastic, which not only verifies that the notch depth of the elastic frequency is consistent with the theoretical design value, but also simulates the basic characteristics of different elastic frequencies.

Key words: elastic suppression, notch filter, verification method, frequency modulation phenomenon

CLC Number:

TP765.2

Su Rixin, Zhang Ou. Research on Verification Method of Missile Elastic Suppression Based on Frequency Compensation[J]. Journal of System Simulation, 2024, 36(5): 1251-1256.

Figures/Tables 6

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References 11

1	张志健, 王小虎, 王铁军. 基于插值DFT的弹体弹性自适应陷波方法[J]. 宇航学报, 2013, 34(9): 1239-1245.
	Zhang Zhijian, Wang Xiaohu, Wang Tiejun. An Interpolated DFT Based Adaptive Notch Filter for Missile Bending Mode Suppression[J]. Journal of Astronautics, 2013, 34(9): 1239-1245.
2	蒲利东, 罗务揆, 严泽洲. 气动伺服弹性系统结构陷幅滤波器优化设计[J]. 工程力学, 2018, 35(4): 235-241.
	Pu Lidong, Luo Wukui, Yan Zezhou. Optimal Design for Notch Filter of Aeroservoelastic Systems[J]. Engineering Mechanics, 2018, 35(4): 235-241.
3	刘莉, 王岩松, 周思达, 等. 考虑弹体弹性的导弹半物理仿真方法与影响分析[J]. 北京航空航天大学学报, 2016, 42(4): 639-645.
	Liu Li, Wang Yansong, Zhou Sida, et al. Hardware-in-the-loop Simulation Method and Influence Analysis of Missiles Considering Body Elasticity[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(4): 639-645.
4	宿常鹏, 王雪梅, 许哲, 等. 导弹姿态控制系统弹性振动抑制问题研究[J]. 弹箭与制导学报, 2019, 39(5): 154-157, 162.
	Su Changpeng, Wang Xuemei, Xu Zhe, et al. Research on Elastic Vibration Suppression of Missile Attitude Control System[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2019, 39(5): 154-157, 162.
5	雷虎民, 楼顺天, 刘兴堂, 等. 六自由度导弹制导系统的建模与仿真研究[J]. 系统仿真学报, 1999, 11(1): 30-33.
	Lei Humin, Lou Shuntian, Liu Xingtang, et al. Six-degree-of-freedom Modelling and Simulation for Missile Guidance Systems[J]. Journal of System Simulation, 1999, 11(1): 30-33.
6	陈文俊. 飞航导弹气动弹性研究工作探讨[J]. 战术导弹技术, 1998(3): 21-28.
	Chen Wenjun. Exploration on Aeroelastic Study for Aerodynamic Missile[J]. Tactical Missile Technology, 1998(3): 21-28.
7	许志, 马宗占, 唐硕. 一种高超声速试飞器助推段主动弹性抑制方法[J]. 宇航学报, 2019, 40(10): 1234-1242.
	Xu Zhi, Ma Zongzhan, Tang Shuo. Active Elastic Control for Boost Stage of a Hypersonic Test Vehicle[J]. Journal of Astronautics, 2019, 40(10): 1234-1242.
8	郜阳, 李彦彬, 王颖, 等. 基于颤振特性的导弹变后掠翼方式研究[J]. 系统仿真学报, 2021, 33(5): 1224-1232.
	Gao Yang, Li Yanbin, Wang Ying, et al. Research on Variable Swept Wing Mode of Missile Based on Flutter Characteristics[J]. Journal of System Simulation, 2021, 33(5): 1224-1232.
9	董小萌, 刘晓东, 王建敏. 摆动喷管推力矢量控制弹性弹体的建模研究[J]. 系统仿真学报, 2014, 26(3): 650-656, 681.
	Dong Xiaomeng, Liu Xiaodong, Wang Jianmin. Modeling Research of Elastic Missile Body with Swing Nozzle Thrust Vector Control[J]. Journal of System Simulation, 2014, 26(3): 650-656, 681.
10	李良, 李友年, 陈星阳. 基于广义最小二乘法的空空导弹幅值滤波器设计方法[J]. 航空兵器, 2020, 27(1): 46-51.
	Li Liang, Li Younian, Chen Xingyang. Amplitude Filter Design of Air-to-air Missile Based on the Generalized Least Square Method[J]. Aero Weaponry, 2020, 27(1): 46-51.
11	郑子元, 林俊, 孔寒雪, 等. 导弹弹性振动在线辨识及自适应抑制[J]. 飞控与探测, 2019, 2(6): 41-47.
	Zheng Ziyuan, Lin Jun, Kong Hanxue, et al. Missile Elastic Vibration Identification and Adaptive Suppression[J]. Flight Control & Detection, 2019, 2(6): 41-47.