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I How to determine the center of gravity of a satellite

  1. Jul 3, 2018 #1
    Hello,

    I am trying to find out how to determine the center of gravity of a CubeSat present in an uniform sphere of radius R, using the initial data given by gyroscopes. The satelitte is equipped with magnetometers, gyroscopes, and accelerometers. By taking into account that the only values I have are angular rates around the three axes, it seems that both the Newton's laws and equations of motion are not enough.
    Does anybody have any idea?

    Thanks in advance!
     
  2. jcsd
  3. Jul 3, 2018 #2
    I'm going to assume that the sphere is massless. Otherwise, we'll be determining the CG (center of gravity) of the combined sphere and satellite.

    Step one would be to allow the sphere to role to a rest on a flat horizontal surface. This would put the CG at it lowest point - directly over the point where the sphere touches the supporting surface. The accelerometers would then tell you how the cube was tilted, thus providing a line where the CG must fall.

    That "low point" on the sphere will also be used as the bottom of the sphere in the next two steps.

    Step two would be to put it on a slippery (frictionless) horizontal surface and hit it with a golf putter - directing a horizontal force on it. The low CG will cause it to spin - and the instrumentation will be able to measure the acceleration and angular velocity.

    Finally, put it onto a golf tee and hit it with a frictionless 9 iron (a 45-degree right ascension angle). Again, the instrumentation will be able to measure the acceleration and angular velocity.

    CG_CubeSat.png

    CG will be along the red line segment.
    The gray blocks are the frictionless golf heads. One a putter, the other a 9-iron (45 degrees).

    Unless the CG is exactly in the middle of the sphere, each golf strike will cause a top spin proportional to the increased velocity.

    Now that I look at it, only one golf strike should be needed to compute the CG. Calculations should be simpler and more accurate with the putter.
     
    Last edited: Jul 3, 2018
  4. Jul 3, 2018 #3

    Khashishi

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    Science Advisor

    Why not measure the center of gravity before launch?
    But nevertheless, I suppose this is a situation where the inverse problem is easier to solve. Given a constant velocity of the center of mass and constant angular momentum, and given the location of the sensors relative to the center of mass, it should be easy to calculate the accelerations and rotations of the sensors as a function of time. You will need to know the location of the sensors relative to each other, at least. Then you can numerically solve for the best fit location of the center of mass based on your data.
     
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