The vibration of flexible structures in spacecraft, such as large space deployable reflectors, solar panels and antenna structure, has a great impact on the normal operation spacecraft. Accurate control is necessary, angular displacement difficulty accurate control. In traditional method, mode good effect suppressing low-order modes, but there overflow. traveling wave modes worse than former, i...

In this article, we first propose a novel maneuvering technique compatible with displacement-consensus-based formation controllers. We show that the can be translated an arbitrary velocity by modifying weights in consensus Laplacian matrix. fact, demonstrate control is particular case of our more general method. then uncover robustness issues undesired steady-state motions and resultant distort...