HSMA:

Path: Missions/Comsat

% Computes the half system moment arms

   Since version 1.
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   Form:
   mAHS = HSMA( mA, id )
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   ------
   Inputs
   ------
   mA           (3,n) Moment arms
   id           (1,n) Thruster ids

   -------
   Outputs
   -------
   mAHS         (3,2) Half System moment arms

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Children:

Math: Linear/Sep

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