By Topic

Simulation of a switched reluctance, More Electric Aircraft power system using a graphical user interface

Sign In

Cookies must be enabled to login.After enabling cookies , please use refresh or reload or ctrl+f5 on the browser for the login options.

Formats Non-Member Member
$31 $13
Learn how you can qualify for the best price for this item!
Become an IEEE Member or Subscribe to
IEEE Xplore for exclusive pricing!
close button

puzzle piece

IEEE membership options for an individual and IEEE Xplore subscriptions for an organization offer the most affordable access to essential journal articles, conference papers, standards, eBooks, and eLearning courses.

Learn more about:

IEEE membership

IEEE Xplore subscriptions

6 Author(s)
Skvarenina, T.L. ; Purdue Univ., West Lafayette, IN, USA ; Pekarek, S. ; Wasynczuk, O. ; Krause, P.C.
more authors

A previous paper described a detailed system model of a More Electric Aircraft power system employing a switched reluctance generator (Skvarenina et al., 1996). That model was written in the Advanced Control System Language (ACSL(R)). The work has been extended to allow two separate phase groups in the switched reluctance machine with independent loads. In addition, the models have been converted to utilize the Graphics Modelle(R) front-end for the ACSL system, which offers flexibility in running different system configurations. The Graphics Modeller and the underlying models for the machine and loads are described, and examples of system studies are shown using various loads, including passive loads, constant power loads, a brushless DC motor, and an electro-hydrostatic actuator. Results from the simulations are presented together with corroborating experimental test results

Published in:

Energy Conversion Engineering Conference, 1997. IECEC-97., Proceedings of the 32nd Intersociety  (Volume:1 )

Date of Conference:

27 Jul-1 Aug 1997