H. Septanto, B. Trilaksono, A. Syaichu-Rohman, R. E. Poetro
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引用次数: 4
Abstract
This paper addresses on the stability analysis of the attitude control system using quaternion-based feedback control law that accommodates arcus-cotangent as a discontinuous elements in the control law. Three argumentations of the asymptotically stability guarantee of the attitude control system are proposed that stated in three theorems. The effectiveness of the proposed control law is shown through numerical simulation.