Line-of-sight based spacecraft attitude and position tracking control

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• 作者：Rakesh R. Warier ; ^{rakeshwarier@sc.iitb.ac.in" class="auth_mail" title="E-mail the corresponding author} ; Arpita Sinha ^{asinha@sc.iitb.ac.in" class="auth_mail" title="E-mail the corresponding author} ; Srikant Sukumar ^{srikant@sc.iitb.ac.in" class="auth_mail" title="E-mail the corresponding author}
• 关键词：Line-of-sight based control ; Spacecraft attitude control ; Spacecraft formation flying ; Coordinate-free attitude control
• 刊名：European Journal of Control
• 出版年：2016
• 出版时间：November 2016
• 年：2016
• 卷：32
• 期：Complete
• 页码：43-53
• 全文大小：2180 K

文摘

This paper considers the problem of formation control of three spacecraft consisting of one leader and two followers. The leader spacecraft controls its attitude and position to track a desired attitude and position trajectory in the Earth Centred Inertial (ECI) frame. Each follower spacecraft tracks a desired relative attitude and relative position trajectory with respect to the leader spacecraft. Absolute attitude control law for the leader and relative attitude control laws for the followers are obtained in terms of line-of-sight vectors between the spacecraft. A relative attitude determination scheme using line-of-sight vectors is also proposed. The state feedback laws proposed in this work guarantee almost global asymptotic stability of the desired closed-loop equilibrium.