TY - GEN
T1 - Design of three axis magnetorquer for microsatellites
AU - Meili, Zhou
AU - Hongyu, Qi
PY - 2013
Y1 - 2013
N2 - Magnetorquer is the device to create the magnetic dipole moment as a result of the interaction between spacecraft moment and the magnetic field. Because the magnetic dipole moment is inversely proportional the third power of the orbit height, magnetorquer is generally used as attitude control system actuator for low earth orbit satellite. In this paper, the design is suitable for the tens of kilograms of micro satellites. In view of low earth orbit satellite locates the region of strong magnetic field intensity, and taking into account the advantages of simple and reliable, magnetorquer must have large output torque, low residual moment, small size, and light weight, this paper is designed to meet these requirements.
AB - Magnetorquer is the device to create the magnetic dipole moment as a result of the interaction between spacecraft moment and the magnetic field. Because the magnetic dipole moment is inversely proportional the third power of the orbit height, magnetorquer is generally used as attitude control system actuator for low earth orbit satellite. In this paper, the design is suitable for the tens of kilograms of micro satellites. In view of low earth orbit satellite locates the region of strong magnetic field intensity, and taking into account the advantages of simple and reliable, magnetorquer must have large output torque, low residual moment, small size, and light weight, this paper is designed to meet these requirements.
KW - large output torque e
KW - low remanence
KW - magnetic dipole moment
KW - microsatellites
UR - https://www.scopus.com/pages/publications/84904561332
U2 - 10.1109/IMCCC.2013.130
DO - 10.1109/IMCCC.2013.130
M3 - 会议稿件
AN - SCOPUS:84904561332
SN - 9780769551227
T3 - Proceedings - 3rd International Conference on Instrumentation and Measurement, Computer, Communication and Control, IMCCC 2013
SP - 579
EP - 582
BT - Proceedings - 3rd International Conference on Instrumentation and Measurement, Computer, Communication and Control, IMCCC 2013
PB - IEEE Computer Society
T2 - 3rd International Conference on Instrumentation and Measurement, Computer, Communication and Control, IMCCC 2013
Y2 - 21 September 2013 through 23 September 2013
ER -