Vibration absorber for a quadcopter?

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minoroctave
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Homework Statement


I am supposed to examine the effectiveness of a vibration absorber design for a quad copter. Attached is a picture of the quad copter and the design; basically each of the spring dampers would be attached to an arm of the copter.
In the case of a single quad copter arm, what would be the primary system and what would be the absorber system?

Homework Equations

The Attempt at a Solution


I know the absorber system is the spring damper and the base plate. but for the primary system, is it just the arm or should i include the motor and the blades?
 
Attachments
  • Two images: top, a photo of a four-rotor quadcopter with white and red arms and black propellers on a wooden table; bottom, a CAD render of a base plate with two pairs of spring-damper units rising from it, each ending in an eyelet.
    quest.png
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How would you normally work it out?
What is is it that you want to stop shaking about?