Active vibration suppression system and method for flexible truss structures based on piezoelectric materials
A technology of truss structure and piezoelectric materials, applied in the direction of piezoelectric effect/electrostrictive or magnetostrictive motors, generators/motors, electrical components, etc., can solve the problem of interference with the normal operation of the attitude control system and the positioning accuracy of spacecraft Influence, nonlinear and other problems, to achieve the effect of obvious vibration suppression, low power consumption, and small effect of natural frequency
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[0017] The present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments.
[0018] like figure 1 As shown, the active vibration suppression system of flexible truss structure vibration based on piezoelectric materials in the present invention includes a main support bar 1 fixed on the ground, a flexible cross bar 2 is fixed on the main support bar 1 and is located on both sides of the flexible cross bar 2 respectively. The left flexible oblique bar 8-1 and the right flexible oblique bar 8-2 are located below the flexible cross bar 2 and are close to the flexible cross bar 2. An installation fixture 3 is fixed on the main support bar 1, and the left side of the other end of the installation fixture 3 passes through The left first rigid rope 4-1 is connected to one end on the short axis side of the left diamond-shaped actuator 5-1, and the other end on the short axis side of the left diamond-shaped actuator 5-1...
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