• 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