Abstract

Most space experiments require very low gravity level. The active vibration control system utilizing electro-magnetic suspensions is being developed to isolate gravity sensitive payload (experimental equipment) from spacecraft vibrational and impulsive disturbances transmitted through rack. Ground model experiment was conducted to verify the control performance of the system with the payload model hanging by the wire to approximate microgravity environment. Results of the experiment showed very good agreement with those of theoretical values and to be applicable to aircraft experiment.

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