DocumentCode
136381
Title
Spacecraft electrical power autonomous management system
Author
Jiang Dongsheng ; Zhang Pei ; Wu Ming
Author_Institution
Beijing Inst. of Spacecraft Syst. Eng., China Acad. of Space Technol., Beijing, China
fYear
2014
fDate
Aug. 31 2014-Sept. 3 2014
Firstpage
1
Lastpage
4
Abstract
Fuses are commonly used in satellites as a main measure for fault isolation. In this paper, a new highly reliable auto management technology of spacecraft power system is studied, the relative research works carried out by Beijing Institute of Spacecraft System Engineering are also illustrated. In the end, three key technologies about electrical autonomous management of spacecraft are concluded, which includes autonomous power management, fault isolation and power dynamic scheduling.
Keywords
aircraft power systems; dynamic scheduling; fault diagnosis; space vehicles; Beijing Institute of Spacecraft System Engineering; auto management technology; autonomous power management; fault isolation; power dynamic scheduling; spacecraft electrical power autonomous management system; spacecraft power system; Circuit faults; Payloads; Power supplies; Power system dynamics; Satellites; Space vehicles; Autonomous Management; power scheduling; spacecraft electrical power;
fLanguage
English
Publisher
ieee
Conference_Titel
Transportation Electrification Asia-Pacific (ITEC Asia-Pacific), 2014 IEEE Conference and Expo
Conference_Location
Beijing
Print_ISBN
978-1-4799-4240-4
Type
conf
DOI
10.1109/ITEC-AP.2014.6940652
Filename
6940652
Link To Document