*HEADING
 : Test Rigid Body Ouput Variables for the ROTARYI element.
 test of ROTARYI elements with various translations and rotations:
  ROTI1 has rotational velocity
  ROTI2 has rotational and translational velocities
  ROTI3 has rot and trans vels, with *TRANSFORM (affects internal U, V)
  ROTI4 has rot and trans vels, with *TRANSFORM and *ORIENTATION
  subsets  1,2,3 share same rotary inertia and mass magnitudes.
*RESTART, WRITE, F=999
**
** roti1
*NODE, NSET=ROTI1
  1, 1.0,  0.0, 0.0
*ELEMENT, TYPE=ROTARYI, ELSET=ROTI1
  1,  1
*ELEMENT, TYPE=MASS, ELSET=ROTI1
  2,  1
*INITIAL CONDITION, TYPE=VELOCITY
 ROTI1, 6, 1.57080
**
** roti2
*NODE, NSET=ROTI2
 11, 1.0,  0.0, 0.0
*ELEMENT, TYPE=ROTARYI, ELSET=ROTI2
 11, 11
*ELEMENT, TYPE=MASS, ELSET=ROTI2
 12, 11
*INITIAL CONDITION, TYPE=VELOCITY
 ROTI2, 1, 10.0
 ROTI2, 6, 1.57080
**
** roti3
*NODE, NSET=ROTI3
 21, 1.0,  0.0, 0.0
*TRANSFORM, NSET=ROTI3
 1.0, 1.0, 0.0, -1.0, 1.0, 0.0
*ELEMENT, TYPE=ROTARYI, ELSET=ROTI3
 21, 21
*ELEMENT, TYPE=MASS, ELSET=ROTI3
 22, 21
** initial conditions are in global system
*INITIAL CONDITION, TYPE=VELOCITY
 ROTI3, 1, 10.0
 ROTI3, 6, 1.57080
**
** roti4
*NODE, NSET=ROTI4
 41, 1.0,  0.0, 0.0
*TRANSFORM, NSET=ROTI4
 1.0, 1.0, 0.0, -1.0, 1.0, 0.0
*ELEMENT, TYPE=ROTARYI, ELSET=ROTI4
 41, 41
*ELEMENT, TYPE=MASS, ELSET=ROTI4
 42, 41
*ROTARY INERTIA, ELSET=ROTI4, ORIENTATION=FORT5
 1.1, 2.2, 3.3
*ORIENTATION, NAME=FORT5
 1.0, 1.0, 0.0, -1.0, 1.0, 0.0
*MASS, ELSET=ROTI4
 0.7, 
*INITIAL CONDITION, TYPE=VELOCITY
 ROTI4, 1, 10.0
 ROTI4, 6, 1.57080
**
*ELSET, ELSET=EALL
 ROTI1, ROTI2, ROTI3
*ROTARY INERTIA, ELSET=EALL
 1.1, 2.2, 3.3
*MASS, ELSET=EALL
 0.7, 
**
*STEP, NLGEOM
*DYNAMIC
 0.1, 1.0
*CONTROLS, PARAMETER=FIELD
 ,,,1.0E-1
*NODE FILE, F=999
COORD, 
V, 
*EL FILE, ELSET=ROTI1, F=999
 XC, 
 UC, 
 VC, 
 RI, 
 HC, 
 HO, 
 MASS, 
 VOL, 
*EL FILE, ELSET=ROTI2, F=999
 XC, 
 UC, 
 VC, 
 RI, 
 HC, 
 HO, 
 MASS, 
 VOL, 
*EL FILE, ELSET=ROTI3, F=999
 XC, 
 UC, 
 VC, 
 RI, 
 HC, 
 HO, 
 MASS, 
 VOL, 
*EL FILE, ELSET=ROTI4, F=999
 XC, 
 UC, 
 VC, 
 RI, 
 HC, 
 HO, 
 MASS, 
 VOL, 
*NODE PRINT, F=0
*EL PRINT, F=0
*END STEP