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Simulation results of vibration control excitation at (a) 0.2, (b) 0.4, (c) 0.6, and (d) 0.8 Hz.

Simulation results of vibration control excitation at (a) 0.2, (b) 0.4, (c) 0.6, and (d) 0.8 Hz.

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With the evolution of space exploration, large flexible appendages have been developed in space structures. External perturbation or attitude maneuvering stimulates the vibration (low frequencies) of the aforementioned structures. In this research, a novel joint mechanism was developed in conjunction with active control to inhibit the low-frequency...