Dipole solution and angular-momentum minimization for two-satellite electromagnetic formation flight
详细信息 查看全文
- 作者：Xian-lin Huang ; Chun Zhang ; zhangchun0055@126.com" class="auth_mail" title="E-mail the corresponding author ; Xiao-jun Ban
- 关键词：Electromagnetic formation flight ; Dipole ; Angular momentum ; Sliding mode control
- 刊名：Acta Astronautica
- 出版年：2016
- 出版时间：February-March 2016
- 年：2016
- 卷：119
- 期：Complete
- 页码：79-86
- 全文大小：774 K
文摘
- •
The obtained dipole solution enables minimizing electromagnetic torques.
- •
The freedom of torque allocation is investigated.
- •
Torque-free formations are presented.
- •
A parameter optimization model is proposed to minimize angular-momentum buildup.