Path: Common/MassProperties
-------------------------------------------------------------------------- Compute inertia, mass and center of mass for a collection of rigid bodies. If no output is specified it will print the results. The cm's must be given in the core frame but the inertias may be given in their own frame and the transformation from the component frame to the core frame given in c. Since version 1. -------------------------------------------------------------------------- Form: [inrT, mT, cMT, inrP, cP] = MassProp( inr, m, cM, u, cName, c ) -------------------------------------------------------------------------- ------ Inputs ------ inr (6,:) Inertia matrices. Each column is [Ixx;Iyy;Izz;Ixy;Ixz;Iyz] Ixy,Ixz and Iyz may be omitted for all bodies. m (1,:) Masses cM (3,:) Center of masses. Each column is [x;y;z] u (3,1) Units 'sgF' = slug-ft^2, 'sgI' = slug-in^2, 'mks' = metric 'inL' = in-lbf-sec^2; cName (:,:) Component name c (9,:) Transformation matrices. Each column is [c(:,1);c(:,2);c(:,3)]; Transforms from the core frame to the element frame ------- Outputs ------- inrT (3,3) Inertia matrix mT (1,1) Mass cMT (3,1) Center of mass inrP (3,3) Inertia matrix in principal axes cP (3,3) Transformation matrix from core to principal axis such that inrP = cP'*inrT*cP --------------------------------------------------------------------------
Common: MassProperties/PrincipalAxes
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