scholarly journals A Novel Frequency-Domain Approach for the Exact Range of Imaginary Spectra and the Stability Analysis of LTI Systems With Two Delays

IEEE Access ◽  
2020 ◽  
Vol 8 ◽  
pp. 36595-36601
Author(s):  
Chengzhi Yuan ◽  
Shuang Song ◽  
Qingbin Gao ◽  
Hamid Reza Karimi ◽  
Libor Pekar ◽  
...  
2014 ◽  
Vol 685 ◽  
pp. 634-637
Author(s):  
Li Zeng ◽  
Jun Wei Wang

A unified frequency-domain approach to analyze the NS (Neimark-Sacker) bifurcations and the period-doubling bifurcations of nonlinear maps with time-delays in the linear feed-forward term is presented. The technique relies on the HBA (harmonic balance approximation, a very important method in data processing ) and feedback systems theory. The expressions of the bifurcation solution and the stability are derived.


2007 ◽  
Vol 17 (04) ◽  
pp. 1355-1366 ◽  
Author(s):  
WENWU YU ◽  
JINDE CAO

In this paper, a general two-neuron model with time delay is considered, where the time delay is regarded as a parameter. It is found that Hopf bifurcation occurs when this delay passes through a sequence of critical value. By analyzing the characteristic equation and using the frequency domain approach, the existence of Hopf bifurcation is determined. The stability of bifurcating periodic solutions are determined by the harmonic balance approach, Nyquist criterion and the graphic Hopf bifurcation theorem. Numerical results are given to justify the theoretical analysis.


2018 ◽  
Vol 2018 (1) ◽  
Author(s):  
Sertaç Erman ◽  
Hulya Kodal Sevindir ◽  
Ali Demir

2011 ◽  
Vol 301-303 ◽  
pp. 1724-1729
Author(s):  
Mei Sa Pang ◽  
Deng Hua Li ◽  
Jun Fang Fan ◽  
Xue Fei Li

The static stability of missile pitching movement is one of the important performances in guidance and control systems. In this paper, a method which consists of the single and double loop longitudinal autopilot using frequency domain approach is proposed to solve the problem efficiently. Single-loop autopilot is used to simplify the system design when the missile is highly static stable; the double-loop autopilot is employed to stabilize the system and improve frequency performance when the missile is static stable or static unstable. Control gain of the system is determined by aerodynamic parameters and frequency domain indexes. The simulation result shows that double-loop autopilot based on frequency domain simplified the system design and improved the stability and robustness of missile system.


Kerntechnik ◽  
2016 ◽  
Vol 81 (1) ◽  
pp. 8-16
Author(s):  
S. J. Kim ◽  
P. N. V. Ha ◽  
J. Y. Lim ◽  
D. H. Hahn ◽  
C. M. Kang

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