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Optimized Design and Analysis of Printed Magnetorquer for a 3-U Nano-Satellite
Journal of Aerospace Engineering ( IF 1.5 ) Pub Date : 2021-09-18 , DOI: 10.1061/(asce)as.1943-5525.0001343 Shoaib Ahmed Khan 1 , Anwar Ali 2 , Yang Shiyou 3 , Shah Fahad 1 , Jijun Tong 4
Journal of Aerospace Engineering ( IF 1.5 ) Pub Date : 2021-09-18 , DOI: 10.1061/(asce)as.1943-5525.0001343 Shoaib Ahmed Khan 1 , Anwar Ali 2 , Yang Shiyou 3 , Shah Fahad 1 , Jijun Tong 4
Affiliation
An active attitude control system using a novel six-layer electromagnetic embedded
printed magnetorquer for a 3-U nanosatellite is presented in this paper. The proposed
design was optimized in terms of size, dissipated power, torque produced, and ...
中文翻译:
3-U纳米卫星印刷磁矩优化设计与分析
本文提出了一种使用新型六层电磁嵌入式印刷磁矩器用于 3-U 纳米卫星的主动姿态控制系统。建议的设计在尺寸、耗散功率、产生的扭矩和……
更新日期:2021-09-19
中文翻译:
3-U纳米卫星印刷磁矩优化设计与分析
本文提出了一种使用新型六层电磁嵌入式印刷磁矩器用于 3-U 纳米卫星的主动姿态控制系统。建议的设计在尺寸、耗散功率、产生的扭矩和……