[email protected]

国际应用数学进展

Advances in International Applied Mathematics

您当前位置:首页 > 精选文章

Advances in International Applied Mathematics. 2024; 6: (2) ; 10.12208/j.aam.20241008 .

Random P bifurcation of vehicle rolling motion system under color noise excitation
色噪声激励下飞行器滚转运动系统的随机P分岔

作者: 马小燕 *

北方民族大学数学与信息科学学院 宁夏银川

*通讯作者: 马小燕,单位:北方民族大学数学与信息科学学院 宁夏银川;

引用本文: 马小燕 色噪声激励下飞行器滚转运动系统的随机P分岔[J]. 国际应用数学进展, 2024; 6: (2) : 1 9-27.
Published: 2024/6/22 19:51:18

摘要

滚转运动在飞行器的横向稳定性中起着关键作用。为了研究随机激励下三角翼飞行器滚转运动的动力学行为,本文在滚转运动模型中引入色噪声激励。首先借助幅值包络随机平均法计算得出FPK方程和振幅响应的平稳概率密度函数。其次,根据奇异性理论,得出系统产生随机P分岔的约束条件。最后,根据该约束条件数值验证了噪声强度与关联时间并不能诱导系统发生随机分岔,而阻尼参数会使系统发生随机P分岔。

关键词: 滚转运动;色噪声;随机平均法;随机P分岔

Abstract

Roll motion plays a key role in the lateral stability of the aircraft. In order to study the dynamic behavior of delta-wing aircraft rolling motion under random excitation, color noise excitation is introduced into the rolling motion model. Firstly, the stationary probability density function of FPK equation and amplitude response is calculated by means of amplitude envelope random average method. Secondly, according to the singularity theory, the constraint conditions for the system to generate random P-bifurcation are obtained. Finally, according to the constraint condition, it is numerically verified that the noise intensity and correlation time can not induce random bifurcation of the system, but the damping parameter can cause random P-bifurcation of the system.

Key words: Rolling movement; Color noise; Stochastic averaging; Random P bifurcation

参考文献 References

[1] 朱位秋. 非线性随机动力学与控制[M]. 北京:科学出版社,2003: 270-280.

[2] 朱位秋. 随机振动. 北京:科学出版社,1998.

[3] ARNOLD L, JONES C K R T, MISCHAIKOW K, et al. Random dynamical systems[M]. Springer Berlin Heidelberg, 1995: 1-30.

[4] 徐伟, 都林. 非线性随机动力系统研究的若干进程[J]. 工程数学学报, 2006, 23 (6): 951-960.

[5] LI Yajie, WU Zhiqiang, WANG Feng, et al. Stochastic P-bifurcation in a generalized Van der Pol oscillator with fractional delayed feedback excited by combined Gaussian white noise excitations[J]. Journal of Low Frequency Noise, Vibration and Active Control, 2021, 40(1): 91-103.

[6] LI Wei, ZHANG Meiting, ZHAO Junfeng. Stochastic bifurcations of generalized Duffing–van der Pol system with fractional derivative under colored noise[J]. Chinese Physics B, 2017, 26(9): 090501.

[7] 邱伟达, 郭永峰. Lévy噪声激励的带有时滞反馈FHN神经元系统的动力学行为研究[J]. 应用力学学报,  2021, 38(05): 2098-2104.

[8] LIU Li, XU Wei, YUE Xiaole, et al. Stochastic response of Duffing-Van der Pol vibro-impact system with viscoelastic term under wide-band excitation[J]. Chaos, Solitons & Fractals, 2017, 104: 748-757.

[9] QIAN Jiamin, CHEN Lincong. Stochastic P-bifurcation analysis of a novel type of unilateral vibro-impact vibration 

[10] WEI Wei, XU Wwei, LIU Jiankang. Stochastic P-bifurcation analysis of a class of nonlinear Markov jump systems under combined harmonic and random excitations[J]. Physica A: Statistical Mechanics and its Applications, 2021, 582: 126246.

[11] Ma Shichao, Wang Liao, Zhang Jinxiu, et al. P-bifurcation phenomena of the non-smooth modified rayleigh-duffing oscillator under the combined action of harmonic excitation and noise perturbation[J]. Physica Scripta, 2023, 98(4): 045211.

[12] 唐佳栋, 娄斌, 叶尚军, 王高峰, 黄志龙. 基于卷积神经网络和松鼠优化算法的机翼结构混合优化设计[J]. 力学季刊, 2022, 43(02): 217-226.

[13] Zhou Hui , Hu Kaiye , Mao Lijun ,et al.Research on planing motion and stability of amphibious aircraft in waves based on cartesian grid finite difference method[J].Ocean engineering, 2023. 

[14] GAO Honggang , HE Ao , GAO Zhenghong ,et al. Flight dynamics characteristics of canard rotor/wing aircraft in helicopter flight mode[J]. Chinese Journal of Aeronautics, 2019, 32(07): 1577-1587.

[15] 付军泉, 史志伟, 耿玺, 朱佳晨, 王力爽, 吴大卫, 潘立军. 基于试验分岔分析的翼身融合飞行器纵向稳定性[J]. 航空学报, 2022, 43(01): 313-321.

[16] 李景奎, 程云开, 齐一蕊, 杨周. 考虑随机参数影响的机翼力学性能数值模拟[J]. 中国工程机械学报, 2020, 18(03): 189-194.

[17] ZHOU Yitao, WU Zhigang , YANG Chao. Intelligent feedforward gust alleviation based on neural network[J]. Chinese Journal of Aeronautics, 2023.

[18] Al-BAHKALI E A, ELKENANI H, SOULI M. Failure and fatigue life due to random vibration in aircraft applications[M]. Multiphysics Simulations in Automotive and Aerospace Applications: Academic Press, 2021: 131-154.

[19] GUO Weili, XU Yong, Li Yongge, et al. Dynamic responses of a conceptual two-dimensional airfoil in hypersonic flows with random perturbations[J]. Journal of Fluids and Structures, 2023, 121: 103920.

[20] HAO Ying, DU Xuewen, HU Yuda, et al. Stochastic P-bifurcation of a 3-DOF airfoil with structural nonlinearity[J]. Journal of Theoretical and Applied Mechanics, 2021, 59(2): 307-317.

[21] MATTRAND C, BOURINET J M. The cross-entropy method for reliability assessment of cracked structures subjected to random Markovian loads[J]. Reliability Engineering & System Safety, 2014, 123: 171-182.

[22] ROBERTS J B, SPANOS P D. Stochastic averaging: an approximate method of solving random vibration problems[J]. International Journal of Non-Linear Mechanics, 1986, 21(2): 111-134.