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
Link To Document :
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