DocumentCode
234594
Title
The design and implement of aviation battery charging and discharging system
Author
Chengtao Cai ; Chao Yang ; Xiaolong Lv
Author_Institution
Coll. of Autom., Harbin Eng. Univ., Harbin, China
fYear
2014
fDate
28-30 July 2014
Firstpage
2947
Lastpage
2952
Abstract
Traditional battery charging equipments usually adopt simple methods such as constant current or constant voltage to charge battery without the ability of monitoring the status of battery in real time in the charging and discharging process. This imprudent approach usually leads to the over-charging as well as irreversible damage to the battery. For dealing with challenge problem, we intend to apply modern power electronics technology, high-frequency inverter technology and discharge depolarization timely technology to overcome those shortcomings mentioned above. At the same time, our major task focused on the hardware design based on DSP controller, including AC to DC circuit, full bridge inverter circuit, driver circuit, the rectifier filter circuit and so on. The simulation and experimental results show that the aviation battery charging equipment we designed can fulfill the practical requirement and has more advantages such as high effective and real-time status detection etc.
Keywords
aircraft power systems; driver circuits; invertors; rectifying circuits; secondary cells; AC to DC circuit; DSP controller; aviation battery charging-discharging system; discharge depolarization; driver circuit; full bridge inverter circuit; high-frequency inverter technology; over-charging; power electronics technology; rectifier filter circuit; Batteries; Bridge circuits; Digital signal processing; Discharges (electric); Inverters; Rectifiers; Voltage control; Aviation battery; charging equipment; full bridge inverter;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (CCC), 2014 33rd Chinese
Conference_Location
Nanjing
Type
conf
DOI
10.1109/ChiCC.2014.6897109
Filename
6897109
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