• DocumentCode
    1724905
  • Title

    Optimal design and implementation of coreless magnetic torque for Nano-satellites

  • Author

    Feng Qian ; Liu Yong ; Li Lizhe ; Pan Quan ; Zhang Chunming ; Yang Guang

  • Author_Institution
    Sch. of Autom., Northwestern Polytech. Univ., Xi´an, China
  • fYear
    2013
  • Firstpage
    5609
  • Lastpage
    5613
  • Abstract
    Magnetorquer is an important, reliable and cost-effective implementation of the device for a Nano-satellite to control the attitude. In this paper, through the study of the design problems of some Nano-satellite´s magnetic torque of China, the design principle has been found that the size of the magnetic moment produced from the coreless magnetic torque is only related to the radius of the wire. Therefore, based on the principle, the paper also gives the optimal design of coreless magnetic torque under the constraints of quality and power consumption. The research has made the coils according to this method and also has designed the coil drive circuit using the principle of Pulse Width Modulation. The experimental results show that this magnetorquer has the qualities of low power consumption, low remanence and low cost, so it could well satisfy the attitude control of Nano-satellite.
  • Keywords
    artificial satellites; attitude control; magnetic moments; torque; China; attitude control; coil drive circuit; coreless magnetic torque; magnetic moment; magnetorquer; nano-satellites; optimal design; pulse width modulation; Attitude control; Coils; Electronic mail; Magnetic circuits; Magnetic cores; Satellites; Torque; attitude control; coil measurement; driver circuit; magnetic torque;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (CCC), 2013 32nd Chinese
  • Conference_Location
    Xi´an
  • Type

    conf

  • Filename
    6640418