Abstract: This paper proposes a novel vibration control method for rigid center–flexible appendage satellites considering actuator/sensor deployments. Initially, we derive the satellite model in planar motion and analyze the impact ...

Abstract: 3RPS/(H) Metamorphic parallel mechanism based on conventional mechanisms is proposed in this study. In contrast to the 3RPS mechanism, the 3RPS/(H) mechanism comprises a novel intermediate metamorphic limb. The different ...

Abstract: This paper addresses the fixed-time, six-degrees-of-freedom control problem for the distributed spacecraft formation system subject to actuator saturation, considering limited communication resources. Since only a fraction ...