Hardware-in-the-loop demonstration on aircraft electrical power system
In recent years, like the automotive industry, aircraft companies have started to develop fully electric aircraft in anticipation of the future. As such, research has been conducted with the goal of achieving a highly efficient aircraft electrical power system (EPS) that also maintains and/or improv...
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2020
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sg-ntu-dr.10356-1387652023-07-07T18:22:38Z Hardware-in-the-loop demonstration on aircraft electrical power system Aw, Meng Kit Wen Changyun School of Electrical and Electronic Engineering Rolls-Royce@NTU Corporate Lab Ooi Gabriel Heo Peng ecywen@ntu.edu.sg Engineering::Electrical and electronic engineering::Power electronics In recent years, like the automotive industry, aircraft companies have started to develop fully electric aircraft in anticipation of the future. As such, research has been conducted with the goal of achieving a highly efficient aircraft electrical power system (EPS) that also maintains and/or improves the fuel efficiency. This project deals with the creation of the EPS of an aircraft fitted with the Rolls Royce Trent 1000 engine. The EPS model will be created using MATLAB/Simulink and interfaced with OPAL-RT for simulation. Parameters are provided my Rolls Royce and used for the EPS model. The results demonstrate the operation of the EPS with simulated hardware inputs. Bachelor of Engineering (Electrical and Electronic Engineering) 2020-05-12T08:17:23Z 2020-05-12T08:17:23Z 2020 Final Year Project (FYP) https://hdl.handle.net/10356/138765 en B1220-191 application/pdf Nanyang Technological University |
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Engineering::Electrical and electronic engineering::Power electronics Aw, Meng Kit Hardware-in-the-loop demonstration on aircraft electrical power system |
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In recent years, like the automotive industry, aircraft companies have started to develop fully electric aircraft in anticipation of the future. As such, research has been conducted with the goal of achieving a highly efficient aircraft electrical power system (EPS) that also maintains and/or improves the fuel efficiency. This project deals with the creation of the EPS of an aircraft fitted with the Rolls Royce Trent 1000 engine. The EPS model will be created using MATLAB/Simulink and interfaced with OPAL-RT for simulation. Parameters are provided my Rolls Royce and used for the EPS model. The results demonstrate the operation of the EPS with simulated hardware inputs. |
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Wen Changyun |
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Wen Changyun Aw, Meng Kit |
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Final Year Project |
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Aw, Meng Kit |
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Aw, Meng Kit |
title |
Hardware-in-the-loop demonstration on aircraft electrical power system |
title_short |
Hardware-in-the-loop demonstration on aircraft electrical power system |
title_full |
Hardware-in-the-loop demonstration on aircraft electrical power system |
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Hardware-in-the-loop demonstration on aircraft electrical power system |
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Hardware-in-the-loop demonstration on aircraft electrical power system |
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hardware-in-the-loop demonstration on aircraft electrical power system |
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Nanyang Technological University |
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2020 |
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https://hdl.handle.net/10356/138765 |
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