Real-time simulation of airplane power distribution system
Airplane power distribution system is developing rapidity in recent years. The concept of a "more electric aircraft (MEA)" and "all electric aircraft (AEA)" represent the trends of airplane power distribution system in the future. Simulation is very important in the desi...
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sg-ntu-dr.10356-651912023-07-04T15:24:43Z Real-time simulation of airplane power distribution system Zhai, Jianyang Wang Peng School of Electrical and Electronic Engineering DRNTU::Engineering::Electrical and electronic engineering::Electric power::Production, transmission and distribution Airplane power distribution system is developing rapidity in recent years. The concept of a "more electric aircraft (MEA)" and "all electric aircraft (AEA)" represent the trends of airplane power distribution system in the future. Simulation is very important in the design of airplane power system. As a certain type of simulation, real-time simulation runs in discrete-time and fixed time step. As the name suggests, real-time simulation runs in the same pace as clock time, which makes rapid control prototyping and hardware in the loop simulation possible on real-time simulators. In this project, real-time simulation is implemented on the modeling of the airplane power system. The complete model of the airplane is built with Simulink, and then simulated on Opal-RT real-time simulators with the assistance of RT-Lab software. The power system model consists of generators, power distribution lines, auxiliary power units, transformer and rectifier units and the loads on both ac and dc buses. The simulation result revealed that it is feasible to run a real-time simulation on airplane power system. However, airplanes commonly use 400Hz ac power system with a great number of power electronic devices adopted. For that reason, the time step must be set extremely small to maintain accuracy in a discrete time simulation. Thus the requirement for the performance of hardware is excessively high in airplane power system simulation. In this project, due to the limitation of hardware, the whole system is separated the power system into smaller scale ones during simulation. The simulation result is reasonable when the time step is set to 0.05 millisecond, and the number of overruns occurred in simulation is acceptable. In further research, it is highly recommended to implement real-time simulation only on single component (control unit, power electric devices, etc.) instead of the whole power system. Master of Science (Power Engineering) 2015-06-15T07:37:21Z 2015-06-15T07:37:21Z 2014 2014 Thesis http://hdl.handle.net/10356/65191 en 86 p. application/pdf |
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DRNTU::Engineering::Electrical and electronic engineering::Electric power::Production, transmission and distribution Zhai, Jianyang Real-time simulation of airplane power distribution system |
description |
Airplane power distribution system is developing rapidity in recent years. The concept
of a "more electric aircraft (MEA)" and "all electric aircraft (AEA)" represent the
trends of airplane power distribution system in the future.
Simulation is very important in the design of airplane power system. As a certain type
of simulation, real-time simulation runs in discrete-time and fixed time step. As the
name suggests, real-time simulation runs in the same pace as clock time, which makes
rapid control prototyping and hardware in the loop simulation possible on real-time
simulators.
In this project, real-time simulation is implemented on the modeling of the airplane
power system. The complete model of the airplane is built with Simulink, and then
simulated on Opal-RT real-time simulators with the assistance of RT-Lab software. The
power system model consists of generators, power distribution lines, auxiliary power
units, transformer and rectifier units and the loads on both ac and dc buses.
The simulation result revealed that it is feasible to run a real-time simulation on
airplane power system. However, airplanes commonly use 400Hz ac power system
with a great number of power electronic devices adopted. For that reason, the time step
must be set extremely small to maintain accuracy in a discrete time simulation. Thus
the requirement for the performance of hardware is excessively high in airplane power
system simulation. In this project, due to the limitation of hardware, the whole system
is separated the power system into smaller scale ones during simulation.
The simulation result is reasonable when the time step is set to 0.05 millisecond, and the number of overruns occurred in simulation is acceptable. In further research, it is
highly recommended to implement real-time simulation only on single component
(control unit, power electric devices, etc.) instead of the whole power system. |
author2 |
Wang Peng |
author_facet |
Wang Peng Zhai, Jianyang |
format |
Theses and Dissertations |
author |
Zhai, Jianyang |
author_sort |
Zhai, Jianyang |
title |
Real-time simulation of airplane power distribution system |
title_short |
Real-time simulation of airplane power distribution system |
title_full |
Real-time simulation of airplane power distribution system |
title_fullStr |
Real-time simulation of airplane power distribution system |
title_full_unstemmed |
Real-time simulation of airplane power distribution system |
title_sort |
real-time simulation of airplane power distribution system |
publishDate |
2015 |
url |
http://hdl.handle.net/10356/65191 |
_version_ |
1772827590139052032 |