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Y2000-62093-V-82 0012536航空配电系统中的子系统集成分析=Analysis of sub-system integration in aircraft power distribution systems[会,英]/Chandrasekaran,S.& Lindner,D.K.//1999 IEEE International Symposium on Circuits and Sys-tems,Vol.5 of 6.—V-82～V-85(PC)讨论了现代飞机的基线电源系统结构稳定性分析。功率电子变换器已广泛应用于现代飞机配电系统。由于其固有的非线性特性,在各个系统集成时可能出现不稳定性。利用分叉分析法识别系统轨道的类型、多重性和稳定性。给出了基线电源系统的完全分叉框图。描述了基线系统的参数值与分叉行为的关系。参8
Y2000-62093-V-00 0012536 Analysis of sub-system integration in aircraft power distribution systems [AC, UK] / Chandrasekaran, S. & Lindner, DK // 1999 IEEE International Symposium on Circuits and Systems, Vol. 5 of 6. -V-82 ~ V-85 (PC) This paper discusses the structural stability analysis of the baseline power system of modern aircraft. Power electronic converter has been widely used in modern aircraft power distribution system. Due to its inherent non-linearity, instability may occur in the integration of individual systems. Bifurcation analysis is used to identify the type, multiplicity and stability of system trajectories. A fully branched block diagram of the baseline power system is given. Describe the relationship between the baseline system parameter values and bifurcation behavior. Participation 8