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Placement of Reaction Control System on a Spacecraft

  1. Sep 14, 2011 #1
    Suppose you have a reaction wheel or a control moment gyroscope on your spacecraft for attitude control. This would be a self contained unit, with 3-axis control. Either device utilizes the conservation of angular momentum, trading angular momentum between the unit and the spaceship frame as needed for attitude control.


    Does the placement of the reaction control unit matter? Should it be as close as possible to the spacecraft's center of mass for the best effect?
  2. jcsd
  3. Sep 14, 2011 #2
  4. Sep 16, 2011 #3


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    I think that placing it on the ends would introduce too much stress in the truss. You would be trying to move the entire mass of the station using only the truss.
  5. Sep 16, 2011 #4
    I agree this would have to be placed near center mass, this would be a point where it would be easiest to have an even spread of balanced forces in as many directions as possible. To place near an end would require more force applied on one side than the other.
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