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
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;
Conference_Titel :
Electrical Machines and Systems (ICEMS), 2011 International Conference on
Conference_Location :
Beijing
Print_ISBN :
978-1-4577-1044-5
DOI :
10.1109/ICEMS.2011.6073534
