Vibration reduction and energy collection integrated device for whole satellite system

The invention relates to the technical field of aerospace engineering, in particular to a whole-satellite system vibration reduction and energy collection integrated device. A guide rod is arranged in a conical shell type satellite adapter shell of the integrated device, a track is arranged on the guide rod, a mass block can move up and down along the track, linear energy collection assemblies arranged on the two sides of the mass block are connected with the side wall of the shell through rotating pairs, and a linear energy collection assembly is further arranged below the mass block. A nonlinear energy collection assembly is arranged above the mass block and is connected with the upper bottom surface of the shell through a guide rod; capacitors of the linear energy acquisition assembly and the nonlinear energy acquisition assembly are electrically connected with the sensor. In a stable state, under the combined action of the linear energy collection assembly and the non-linear energy collection assembly, th