DocumentCode :
2791856
Title :
Energy recovery from landing aircraft
Author :
Zulkifli, Shamsul Aizam
Author_Institution :
Dept. of Aeronaut. & Automotive Eng., Loughborough Univ., Loughborough, UK
fYear :
2012
fDate :
25-28 June 2012
Firstpage :
93
Lastpage :
100
Abstract :
This paper describes, the control strategy for energy recovery from landing aircraft. Energy from landing aircraft can be collected and changed to electrical power by using several power electronics devices. Each power electronics devices has their own control strategy, that will change from one type of input to other output. The controllers that have been used are included the H control and PI control. The simulations have been done in MATLAB program and the results show that the energy from landing aircraft can be converted and transferred to electrical power.
Keywords :
H control; PI control; energy storage; power convertors; H∞ control; MATLAB program; PI control; energy recovery; landing aircraft; power electronics devices; Aerospace electronics; Aircraft; Equations; Mathematical model; Power electronics; Supercapacitors;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Power Electronics for Distributed Generation Systems (PEDG), 2012 3rd IEEE International Symposium on
Conference_Location :
Aalborg
Print_ISBN :
978-1-4673-2021-4
Electronic_ISBN :
978-1-4673-2022-1
Type :
conf
DOI :
10.1109/PEDG.2012.6253985
Filename :
6253985
Link To Document :
بازگشت