Amplitude death, oscillation death, and periodic regimes in dynamically coupled Landau–Stuart oscillators with and without distributed delay

2021 ◽  
Vol 187 ◽  
pp. 30-50
Author(s):  
Ryan Roopnarain ◽  
S. Roy Choudhury
2011 ◽  
Vol 84 (2) ◽  
pp. 307-315 ◽  
Author(s):  
Y. N. Kyrychko ◽  
K. B. Blyuss ◽  
E. Schöll

Author(s):  
Y. N. Kyrychko ◽  
K. B. Blyuss ◽  
E. Schöll

This paper studies the effects of distributed-delay coupling on the dynamics in a system of non-identical coupled Stuart–Landau oscillators. For uniform and gamma delay distribution kernels, the conditions for amplitude death are obtained in terms of average frequency, frequency detuning and the parameters of the coupling, including coupling strength and phase, as well as the mean time delay and the width of the delay distribution. To gain further insights into the dynamics inside amplitude death regions, the eigenvalues of the corresponding characteristic equations are computed numerically. Oscillatory dynamics of the system is also investigated, using amplitude and phase representation. Various branches of phase-locked solutions are identified, and their stability is analysed for different types of delay distributions.


Author(s):  
Dawei Wu ◽  
Jun Zhou ◽  
Hui Ye

In this article, the high angle of attack (AOA) maneuver control problem is studied under multiple disturbances and uncertainties. For the first time, the switched distributed delay is constructed to characterize the unsteady aerodynamics. Based on neural networks (NNs) and hyperbolic tangent function, the disturbance observer technique is extended to the nonstrict-feedback system control. To handle the switching problem, time-delay problem, and nonstrict-feedback problem caused by switched distributed delay terms, the Lyapunov–Krasovskii (LK) functional method and a variable separation method are cleverly combined. The proposed LK function can relax the constraints on time-varying delay. Finally, a disturbance observer–based neural finite-time prescribed performance flight control law is developed to improve the flight performance at high AOA, and its effectiveness has been verified through rigorous theoretical analysis and simulation experiments.


Author(s):  
Abdelhak Djebabla ◽  
Abdelbaki Choucha ◽  
Djamel Ouchenane ◽  
Khaled Zennir

2019 ◽  
Vol 27 (10) ◽  
pp. 1963-1973 ◽  
Author(s):  
Shen Yan ◽  
Mouquan Shen ◽  
Sing Kiong Nguang ◽  
Guangming Zhang ◽  
Liruo Zhang

2000 ◽  
Vol 84 (23) ◽  
pp. 5312-5315 ◽  
Author(s):  
R. Herrero ◽  
M. Figueras ◽  
J. Rius ◽  
F. Pi ◽  
G. Orriols

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