DocumentCode
2275207
Title
Design of a novel DC power feedback electronic load
Author
Xie, Zhanming ; Guo, Hong
Author_Institution
Sch. of Autom. Sci. & Electr. Eng., Beijing Univ. of Aeronaut. & Astronaut., Beijing, China
fYear
2011
fDate
20-23 Aug. 2011
Firstpage
1
Lastpage
3
Abstract
A novel electronic load with the characteristic of DC power feedback is put forward. The load is specially designed for aircraft applying. The model of the load is analyzed and parameters are designed. A practical load structure is presented in this paper and the system stability is discussed. Energy may be saved more than 80% using the load when choosing a suitable feedback resistance. Experiment is made to prove the result.
Keywords
aircraft power systems; energy conservation; feedback; load (electric); parameter estimation; power system stability; DC power feedback electronic load design; aircraft application; energy saving; feedback resistance; parameter design; system stability; Aerospace electronics; Aircraft; Impedance; Load modeling; Mathematical model; Power supplies; Stability analysis;
fLanguage
English
Publisher
ieee
Conference_Titel
Electrical Machines and Systems (ICEMS), 2011 International Conference on
Conference_Location
Beijing
Print_ISBN
978-1-4577-1044-5
Type
conf
DOI
10.1109/ICEMS.2011.6073534
Filename
6073534
Link To Document