非ホロノミック拘束に着目した剛体衛星軌道のフィードバック制御

抄録

This study proposes a feedback control law for orbital parameters of a coplanar rigid satellite system. The governing equations are denoted as ‘Symmetrical Affine System’ with three variables and two control inputs, which is guaranteed to be locally controllable. However, because of time-variant parameters included in the governing equations, previously proposed feedback control laws cannot be directly applied. Therefore, in this paper, a novel feedback control law to simultaneously control plural orbital parameters is proposed. Finally the effectiveness of the proposed control law is validated through numerical simulations.