Simulation of MADMEL Power Systems Components 981258
Detailed computer models of system components for More Electric Aircraft have been developed using the Advanced Control System Language (ACSL) and its graphical front-end, Graphic Modeller. Among the devices modeled are a wound-rotor synchronous generator with parallel bridge-rectifier outputs, a switched-reluctance generator, and various loads including a DC-DC converter, an inverter-driven induction motor, and an electro-hydrostatic actuator. Results from the simulations are presented together with corroborating experimental test results.
Citation: Skvarenina, T., Wasynczuk, O., Krause, P., and Pekarek, S., "Simulation of MADMEL Power Systems Components," SAE Technical Paper 981258, 1998, https://doi.org/10.4271/981258. Download Citation
Author(s):
Timothy L. Skvarenina, Oleg Wasynczuk, Paul C. Krause, Steven D. Pekarek
Affiliated:
Purdue University
Pages: 8
Event:
Aerospace Power Systems Conference
ISSN:
0148-7191
e-ISSN:
2688-3627
Also in:
Aerospace Power Systems Conference Proceedings-P-322, SAE 1998 Transactions - Journal of Aerospace-V107-1
Related Topics:
Computer simulation
Electric aircraft
Control systems
Simulation and modeling
Sensors and actuators
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