DocumentCode :
171082
Title :
Electrical power source model on board of a more electric aircraft
Author :
Ureche, Eduard-Ionut
Author_Institution :
Aerosp. Eng. Ph.D. Sch., Univ. “Politeh.” of Bucharest, Bucharest, Romania
fYear :
2014
fDate :
23-25 Oct. 2014
Firstpage :
1
Lastpage :
6
Abstract :
This paper presents a modeling study of an electrical power source for more electric aircrafts. It was designed with a PI (proportional-integrator) automated control for dq currents of the electrical machine, using the non-linear model of it. Using the dimensionless linear model, it was designed an optimal control structure based on a quadratic quality criterion (LQR) to validate the theoretical results and the MATLAB/SIMULINK model was created for this purpose. With this model were plotted the features which express the dynamic state variables of the system.
Keywords :
PI control; aircraft power systems; optimal control; MATLAB model; PI automated control; SIMULINK model; dimensionless linear model; dq currents; dynamic state variables; electric aircraft; electrical machine; electrical power source model; nonlinear model; optimal control structure; proportional-integrator automated control; quadratic quality criterion; Aircraft; Atmospheric modeling; Equations; Generators; Mathematical model; Rotors; Torque; dq coordinates; electrical source; more electric aircraft;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Applied and Theoretical Electricity (ICATE), 2014 International Conference on
Conference_Location :
Craiova
Type :
conf
DOI :
10.1109/ICATE.2014.6972686
Filename :
6972686
Link To Document :
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