Modeling Considerations and Stability Analysis of Aerospace Power Systems with Hybrid AC/DC Distribution

2006-01-3038

11/07/2006

Authors Abstract
Content
The modeling and simulation of electrical power systems has become a primary design tool for the synthesis of aerospace power systems with hybrid AC/DC distribution. Although in the past the use of extensive time domain simulations using detailed models has been favored, the need to study stability and associated phenomena in this type of power systems-having a high penetration of power electronics loads-has transformed the modeling requirements for aerospace applications. This paper explores different modeling aspects required to study both small-signal and large-signal stability in these systems, providing insight into the development of key system component models-variable frequency generators, line-commutated converters, PWM motor drives and constant power loads, as well as the theoretical foundations based on the Generalized Nyquist Criterion and the Lyapunov Direct and Indirect Methods to fully assess the stability conditions of these power systems. Modeling and design examples using Matlab/Simulink are used for verification purposes.
Meta TagsDetails
DOI
https://doi.org/10.4271/2006-01-3038
Pages
16
Citation
Burgos, R., Rosado, S., Wang, F., Boroyevich, D. et al., "Modeling Considerations and Stability Analysis of Aerospace Power Systems with Hybrid AC/DC Distribution," SAE Technical Paper 2006-01-3038, 2006, https://doi.org/10.4271/2006-01-3038.
Additional Details
Publisher
Published
Nov 7, 2006
Product Code
2006-01-3038
Content Type
Technical Paper
Language
English