MBDynCaseJose.mbd .mov

# Conflicts:
#	testapp/OndselSolver.cpp
This commit is contained in:
Aik-Siong Koh
2023-11-14 15:18:10 -07:00
parent 9e9a930622
commit aa8d647ce8
27 changed files with 6437 additions and 380 deletions

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-----------------------------------------------------------------------------
# [Data Block]
begin: data;
problem: initial value;
end: data;
#-----------------------------------------------------------------------------
# [Problem Block]
begin: initial value;
initial time: 0.0;
final time: 8.0;
time step: 0.01;
max iterations: 100;
tolerance: 1e-06;
derivatives tolerance: 0.0001;
derivatives max iterations: 100;
derivatives coefficient: auto;
end: initial value;
#-----------------------------------------------------------------------------
# [Control Data Block]
begin: control data;
max iterations: 1000;
default orientation: euler321;
omega rotates: no;
print: none;
initial stiffness: 1.0, 1.0;
structural nodes: 4;
rigid bodies: 3;
joints: 6;
end: control data;
#-----------------------------------------------------------------------------
# [Design Variables]
#Generic bodies
#body: 2
set: integer body_2 = 2; #body label
set: real mass_2 = 3.805252376198168; #mass [kg]
set: real volume_2 = 0.0004816775159744516; #volume [m^3]
#body: 3
set: integer body_3 = 3; #body label
set: real mass_3 = 15.238784954845523; #mass [kg]
set: real volume_3 = 0.0019289601208665218; #volume [m^3]
#body: 4
set: integer body_4 = 4; #body label
set: real mass_4 = 2.865603331977783; #mass [kg]
set: real volume_4 = 0.0003627345989845295; #volume [m^3]
#Nodes
#node: 1
set: integer structural_node_1 = 1; #node label
#node: 2
set: integer structural_node_2 = 2; #node label
#node: 3
set: integer structural_node_3 = 3; #node label
#node: 4
set: integer structural_node_4 = 4; #node label
#Joints
#joint: 1
set: integer joint_1 = 1; #joint label
#joint: 2
set: integer joint_2 = 2; #joint label
#joint: 3
set: integer joint_3 = 3; #joint label
#joint: 4
set: integer joint_4 = 4; #joint label
#joint: 5
set: integer joint_5 = 5; #joint label
#joint: 6
set: integer joint_6 = 6; #joint label
#Nodes: initial conditions
#node: 1
set: real Px_1 = -0.06210573361337854; #X component of the absolute position [m]
set: real Py_1 = 0.048526435375479564; #Y component of the absolute position [m]
set: real Pz_1 = -4.033966837940965e-17; #Z component of the absolute position [m]
set: real Vx_1 = 0.0; #X component of the absolute velocity [m/s]
set: real Vy_1 = 0.0; #Y component of the absolute velocity [m/s]
set: real Vz_1 = 0.0; #Z component of the absolute velocity [m/s]
set: real Wx_1 = 0.0; #X component of the absolute angular velocity [rad/s]
set: real Wy_1 = 0.0; #Y component of the absolute angular velocity [rad/s]
set: real Wz_1 = 0.0; #Z component of the absolute angular velocity [rad/s]
#node: 2
set: real Px_2 = 0.011666006676941875; #X component of the absolute position [m]
set: real Py_2 = 0.15999999999999778; #Y component of the absolute position [m]
set: real Pz_2 = -1.2084363289349542e-19; #Z component of the absolute position [m]
set: real Vx_2 = 0.0; #X component of the absolute velocity [m/s]
set: real Vy_2 = 0.0; #Y component of the absolute velocity [m/s]
set: real Vz_2 = 0.0; #Z component of the absolute velocity [m/s]
set: real Wx_2 = 0.0; #X component of the absolute angular velocity [rad/s]
set: real Wy_2 = 0.0; #Y component of the absolute angular velocity [rad/s]
set: real Wz_2 = 0.0; #Z component of the absolute angular velocity [rad/s]
#node: 3
set: real Px_3 = 0.2111281366952498; #X component of the absolute position [m]
set: real Py_3 = 0.16; #Y component of the absolute position [m]
set: real Pz_3 = -2.0217697810416158e-18; #Z component of the absolute position [m]
set: real Vx_3 = 0.0; #X component of the absolute velocity [m/s]
set: real Vy_3 = 0.0; #Y component of the absolute velocity [m/s]
set: real Vz_3 = 0.0; #Z component of the absolute velocity [m/s]
set: real Wx_3 = 0.0; #X component of the absolute angular velocity [rad/s]
set: real Wy_3 = 0.0; #Y component of the absolute angular velocity [rad/s]
set: real Wz_3 = 0.0; #Z component of the absolute angular velocity [rad/s]
#node: 4
set: real Px_4 = -0.1812239275015207; #X component of the absolute position [m]
set: real Py_4 = 0.16000000169909329; #Y component of the absolute position [m]
set: real Pz_4 = -4.340477856936436e-12; #Z component of the absolute position [m]
set: real Vx_4 = 0.0; #X component of the absolute velocity [m/s]
set: real Vy_4 = 0.0; #Y component of the absolute velocity [m/s]
set: real Vz_4 = 0.0; #Z component of the absolute velocity [m/s]
set: real Wx_4 = 0.0; #X component of the absolute angular velocity [rad/s]
set: real Wy_4 = 0.0; #Y component of the absolute angular velocity [rad/s]
set: real Wz_4 = 0.0; #Z component of the absolute angular velocity [rad/s]
#-----------------------------------------------------------------------------
# [Intermediate Variables]
#Moments of inertia and relative center of mass
#body 2:
set: real Ixx_2 = 0.031674420620509; #moment of inertia [kg*m^2]
set: real Iyy_2 = 0.029604112147595; #moment of inertia [kg*m^2]
set: real Izz_2 = 0.002867529429125; #moment of inertia [kg*m^2]
set: real Rx_2 = 0.0; #X component of the relative center of mass [m]
set: real Ry_2 = 0.0; #Y component of the relative center of mass [m]
set: real Rz_2 = 2.0843632893495426e-20; #Z component of the relative center of mass [m]
#body 3:
set: real Ixx_3 = 0.09813066341583701; #moment of inertia [kg*m^2]
set: real Iyy_3 = 0.095433846761275; #moment of inertia [kg*m^2]
set: real Izz_3 = 0.077043262824289; #moment of inertia [kg*m^2]
set: real Rx_3 = 0.0; #X component of the relative center of mass [m]
set: real Ry_3 = 0.0; #Y component of the relative center of mass [m]
set: real Rz_3 = 2.1769781041615487e-20; #Z component of the relative center of mass [m]
#body 4:
set: real Ixx_4 = 0.010133521085753; #moment of inertia [kg*m^2]
set: real Iyy_4 = 0.006853402672398001; #moment of inertia [kg*m^2]
set: real Izz_4 = 0.00669113151275; #moment of inertia [kg*m^2]
set: real Rx_4 = 0.0; #X component of the relative center of mass [m]
set: real Ry_4 = 0.0; #Y component of the relative center of mass [m]
set: real Rz_4 = -4.306356366563123e-20; #Z component of the relative center of mass [m]
#-----------------------------------------------------------------------------
# [Nodes Block]
begin: nodes;
structural: structural_node_1,
static,
Px_1, Py_1, Pz_1, #<absolute_position> [m]
3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0, #<absolute_orientation_matrix>
Vx_1, Vy_1, Vz_1, #<absolute_velocity> [m/s]
Wx_1, Wy_1, Wz_1; #<absolute_angular_velocity> [rad/s]
structural: structural_node_2,
dynamic,
Px_2, Py_2, Pz_2, #<absolute_position> [m]
3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0, #<absolute_orientation_matrix>
Vx_2, Vy_2, Vz_2, #<absolute_velocity> [m/s]
Wx_2, Wy_2, Wz_2; #<absolute_angular_velocity> [rad/s]
structural: structural_node_3,
dynamic,
Px_3, Py_3, Pz_3, #<absolute_position> [m]
3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0, #<absolute_orientation_matrix>
Vx_3, Vy_3, Vz_3, #<absolute_velocity> [m/s]
Wx_3, Wy_3, Wz_3; #<absolute_angular_velocity> [rad/s]
structural: structural_node_4,
dynamic,
Px_4, Py_4, Pz_4, #<absolute_position> [m]
3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0, #<absolute_orientation_matrix>
Vx_4, Vy_4, Vz_4, #<absolute_velocity> [m/s]
Wx_4, Wy_4, Wz_4; #<absolute_angular_velocity> [rad/s]
end: nodes;
#-----------------------------------------------------------------------------
# [Elements Block]
begin: elements;
#-----------------------------------------------------------------------------
# [Bodies]
body: body_2,
structural_node_2, #<node_label>
mass_2, #<mass> [kg]
Rx_2, Ry_2, Rz_2, #<relative_center_of_mass> [m]
diag, Ixx_2, Iyy_2, Izz_2, #<inertia matrix> [kg*m^2]
orientation, 3, 1.0, 0.0, 0.0, 2, 0.0, 0.9999999999999999, 9.62964972193618e-35;
body: body_3,
structural_node_3, #<node_label>
mass_3, #<mass> [kg]
Rx_3, Ry_3, Rz_3, #<relative_center_of_mass> [m]
diag, Ixx_3, Iyy_3, Izz_3, #<inertia matrix> [kg*m^2]
orientation, 3, 0.0, 0.0, 1.0, 2, 1.0, 0.0, 0.0;
body: body_4,
structural_node_4, #<node_label>
mass_4, #<mass> [kg]
Rx_4, Ry_4, Rz_4, #<relative_center_of_mass> [m]
diag, Ixx_4, Iyy_4, Izz_4, #<inertia matrix> [kg*m^2]
orientation, 3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0;
#-----------------------------------------------------------------------------
# [Joints]
joint: joint_1,
clamp,
structural_node_1, #<node_label>
-0.06210573361337854, 0.048526435375479564, -4.033966837940965e-17, #<absolute_pin_position> [m]
3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0; #<absolute_orientation_matrix>
joint: joint_2,
axial rotation,
structural_node_1, #<node_1_label>
0.2521057336133785, 0.11147356462452043, 0.13500000000000004, #<relative_offset_1> [m]
orientation, 3, 0.0, 0.0, 1.0, 2, -1.0, 2.220446049250313e-16, 0.0, #<relative_orientation_matrix_1>
structural_node_3, #<node_2_label>
-0.021128136695249794, 0.0, 0.135, #<relative_offset_2> [m]
orientation, 3, 0.0, 0.0, 1.0, 2, -1.0, 2.220446049250313e-16, 0.0, #<relative_orientation_matrix_2>
string, "model::drive(1, Time)"; #<angular_velocity> [rad/s]
joint: joint_3,
revolute hinge,
structural_node_2, #<node_1_label>
0.08833399332305812, 2.2168933355715126e-15, 0.065, #<relative_position_1> [m]
orientation, 3, 0.0, 0.0, 1.0, 2, -1.0, 2.220446049250313e-16, 0.0, #<relative_pin_orientation_matrix_1>
structural_node_3, #<node_2_label>
-0.11112813669524979, 0.0, 0.065, #<relative_position_2> [m]
orientation, 3, 0.0, 0.0, 1.0, 2, -1.0, 2.220446049250313e-16, 0.0; #<relative_pin_orientation_matrix_2>
joint: joint_4,
prismatic,
structural_node_1, #<node_1_label>
orientation, 3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0, #relative_orientation_matrix_1>
structural_node_4, #<node_2_label>
orientation, 3, 0, 0, 1, 2, 0, 1, 0; #relative_orientation_matrix_2>
joint: joint_5,
in line,
structural_node_1, #<node_1_label>
0.0, 0.11147355803101042, 2.4118673970779456e-17, #<relative_line_position> [m]
3, -1.0, 1.1102230246251565e-16, -2.220446049250313e-16, 2, -1.1102230246251565e-16, 0.0, 1.0, #<relative_orientation>
structural_node_4, #<node_2_label>
offset, 0.0, -8.292603282173139e-09, 4.340448411165876e-12; #<relative_offset> [m]
joint: joint_6,
in line,
structural_node_2, #<node_1_label>
-0.1616660066769419, 2.2168933355715126e-15, 0.0, #<relative_line_position> [m]
3, 0.0, -0.0, -1.0, 2, -1.0, -2.220446049250313e-16, 0.0, #<relative_orientation>
structural_node_4, #<node_2_label>
offset, 0.031223927501520705, -1.69909327496498e-09, 7.275957614183426e-15; #<relative_offset> [m]
#-----------------------------------------------------------------------------
# [Drive callers]
drive caller: 1, name,"drive:1", ramp, 10.0, 0.0, 1.0, 0.0;
end: elements;

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######################################################################################################################
# MBDyn is a free and open-source general purpose multi-body dynamics software. See https://www.mbdyn.org/ for details.
# This input file was automatically generated by the FreeCAD "MBD workbench".
# To learn more about MBDyn input files, you can visit the website: https://www.sky-engin.jp/en/MBDynTutorial/index.html
# Details about the structure of input files can be studied in the input file manuals: https://www.mbdyn.org/?Software_Download
# Although MBDyn has already reached a mature stage and is used by several industries,
# the FreeCAD dynamics workbench is still under development, and it is likely to have bugs.
# Please be aware of this fact before you use this input file for any critical application.
# If you think you have found a bug or have any suggestion, please send your comments to Jose Egas:
# josegegas@gmail.com
######################################################################################################################
#-----------------------------------------------------------------------------
# [Data Block]
begin: data;
problem: initial value;
end: data;
#-----------------------------------------------------------------------------
# [Problem Block]
begin: initial value;
initial time: 0.0;
final time: 8.0;
time step: 0.1;
max iterations: 100;
tolerance: 1e-06;
derivatives tolerance: 0.0001;
derivatives max iterations: 100;
derivatives coefficient: auto;
end: initial value;
#-----------------------------------------------------------------------------
# [Control Data Block]
begin: control data;
max iterations: 1000;
default orientation: euler321;
omega rotates: no;
print: none;
initial stiffness: 1.0, 1.0;
structural nodes: 4;
rigid bodies: 3;
joints: 7;
end: control data;
#-----------------------------------------------------------------------------
# [Design Variables]
#Generic bodies
#body: 2
set: integer body_2 = 2; #body label
set: real mass_2 = 1.4486361883511716; #mass [kg]
set: real volume_2 = 0.0001833716694115407; #volume [m^3]
#body: 3
set: integer body_3 = 3; #body label
set: real mass_3 = 2.85294865570677; #mass [kg]
set: real volume_3 = 0.00036113274122870505; #volume [m^3]
#body: 4
set: integer body_4 = 4; #body label
set: real mass_4 = 10.859427202622147; #mass [kg]
set: real volume_4 = 0.0013746110383066007; #volume [m^3]
#Nodes
#node: 1
set: integer structural_node_1 = 1; #node label
#node: 2
set: integer structural_node_2 = 2; #node label
#node: 3
set: integer structural_node_3 = 3; #node label
#node: 4
set: integer structural_node_4 = 4; #node label
#Joints
#joint: 1
set: integer joint_1 = 1; #joint label
#joint: 2
set: integer joint_2 = 2; #joint label
#joint: 3
set: integer joint_3 = 3; #joint label
#joint: 4
set: integer joint_4 = 4; #joint label
#joint: 5
set: integer joint_5 = 5; #joint label
#joint: 6
set: integer joint_6 = 6; #joint label
#joint: 7
set: integer joint_7 = 7; #joint label
#Nodes: initial conditions
#node: 1
set: real Px_1 = -0.121; #X component of the absolute position [m]
set: real Py_1 = -8.796847998598882e-19; #Y component of the absolute position [m]
set: real Pz_1 = -0.08; #Z component of the absolute position [m]
set: real Vx_1 = 0.0; #X component of the absolute velocity [m/s]
set: real Vy_1 = 0.0; #Y component of the absolute velocity [m/s]
set: real Vz_1 = 0.0; #Z component of the absolute velocity [m/s]
set: real Wx_1 = 0.0; #X component of the absolute angular velocity [rad/s]
set: real Wy_1 = 0.0; #Y component of the absolute angular velocity [rad/s]
set: real Wz_1 = 0.0; #Z component of the absolute angular velocity [rad/s]
#node: 2
set: real Px_2 = -0.015; #X component of the absolute position [m]
set: real Py_2 = 0.092; #Y component of the absolute position [m]
set: real Pz_2 = 0.008; #Z component of the absolute position [m]
set: real Vx_2 = 0.0; #X component of the absolute velocity [m/s]
set: real Vy_2 = 0.0; #Y component of the absolute velocity [m/s]
set: real Vz_2 = 0.0; #Z component of the absolute velocity [m/s]
set: real Wx_2 = 0.0; #X component of the absolute angular velocity [rad/s]
set: real Wy_2 = 0.0; #Y component of the absolute angular velocity [rad/s]
set: real Wz_2 = 0.0; #Z component of the absolute angular velocity [rad/s]
#node: 3
set: real Px_3 = 0.088; #X component of the absolute position [m]
set: real Py_3 = -0.055; #Y component of the absolute position [m]
set: real Pz_3 = 0.05; #Z component of the absolute position [m]
set: real Vx_3 = 0.0; #X component of the absolute velocity [m/s]
set: real Vy_3 = 0.0; #Y component of the absolute velocity [m/s]
set: real Vz_3 = 0.0; #Z component of the absolute velocity [m/s]
set: real Wx_3 = 0.0; #X component of the absolute angular velocity [rad/s]
set: real Wy_3 = 0.0; #Y component of the absolute angular velocity [rad/s]
set: real Wz_3 = 0.0; #Z component of the absolute angular velocity [rad/s]
#node: 4
set: real Px_4 = 0.3200000010688326; #X component of the absolute position [m]
set: real Py_4 = 1.4796688528733327e-10; #Y component of the absolute position [m]
set: real Pz_4 = 0.04999999225971574; #Z component of the absolute position [m]
set: real Vx_4 = 0.0; #X component of the absolute velocity [m/s]
set: real Vy_4 = 0.0; #Y component of the absolute velocity [m/s]
set: real Vz_4 = 0.0; #Z component of the absolute velocity [m/s]
set: real Wx_4 = 0.0; #X component of the absolute angular velocity [rad/s]
set: real Wy_4 = 0.0; #Y component of the absolute angular velocity [rad/s]
set: real Wz_4 = 0.0; #Z component of the absolute angular velocity [rad/s]
#-----------------------------------------------------------------------------
# [Intermediate Variables]
#Moments of inertia and relative center of mass
#body 2:
set: real Ixx_2 = 0.0012769356301204219; #moment of inertia [kg*m^2]
set: real Ixy_2 = 4.67e-20; #moment of inertia [kg*m^2]
set: real Ixz_2 = -0.0009495625871945231; #moment of inertia [kg*m^2]
set: real Iyx_2 = 4.67e-20; #moment of inertia [kg*m^2]
set: real Iyy_2 = 0.0028717510150978666; #moment of inertia [kg*m^2]
set: real Iyz_2 = 4.4900000000000004e-20; #moment of inertia [kg*m^2]
set: real Izx_2 = -0.0009495625871945231; #moment of inertia [kg*m^2]
set: real Izy_2 = 4.4900000000000004e-20; #moment of inertia [kg*m^2]
set: real Izz_2 = 0.002296471669735477; #moment of inertia [kg*m^2]
set: real Rx_2 = -0.03260146715730948; #X component of the relative center of mass [m]
set: real Ry_2 = 0.0; #Y component of the relative center of mass [m]
set: real Rz_2 = -0.028286762255221056; #Z component of the relative center of mass [m]
#body 3:
set: real Ixx_3 = 0.0019563103180210077; #moment of inertia [kg*m^2]
set: real Ixy_3 = -7.580852e-16; #moment of inertia [kg*m^2]
set: real Ixz_3 = 5.386829000000001e-16; #moment of inertia [kg*m^2]
set: real Iyx_3 = -7.580852e-16; #moment of inertia [kg*m^2]
set: real Iyy_3 = 0.03371514809951082; #moment of inertia [kg*m^2]
set: real Iyz_3 = -4.95494e-17; #moment of inertia [kg*m^2]
set: real Izx_3 = 5.386829000000001e-16; #moment of inertia [kg*m^2]
set: real Izy_3 = -4.95494e-17; #moment of inertia [kg*m^2]
set: real Izz_3 = 0.03383792198797204; #moment of inertia [kg*m^2]
set: real Rx_3 = 7.87281351222191e-15; #X component of the relative center of mass [m]
set: real Ry_3 = 1.0302869668521452e-15; #Y component of the relative center of mass [m]
set: real Rz_3 = -0.024999999999998045; #Z component of the relative center of mass [m]
#body 4:
set: real Ixx_4 = 0.07706742098795094; #moment of inertia [kg*m^2]
set: real Ixy_4 = 8.01291908309e-10; #moment of inertia [kg*m^2]
set: real Ixz_4 = -1.2135214817691901e-08; #moment of inertia [kg*m^2]
set: real Iyx_4 = 8.01291908309e-10; #moment of inertia [kg*m^2]
set: real Iyy_4 = 0.06635181579849883; #moment of inertia [kg*m^2]
set: real Iyz_4 = -3.32678908792e-11; #moment of inertia [kg*m^2]
set: real Izx_4 = -1.2135214817691901e-08; #moment of inertia [kg*m^2]
set: real Izy_4 = -3.32678908792e-11; #moment of inertia [kg*m^2]
set: real Izz_4 = 0.06179235045624136; #moment of inertia [kg*m^2]
set: real Rx_4 = 0.045580834634119355; #X component of the relative center of mass [m]
set: real Ry_4 = 2.0299354041266675e-10; #Y component of the relative center of mass [m]
set: real Rz_4 = -1.2562251448855477e-08; #Z component of the relative center of mass [m]
#-----------------------------------------------------------------------------
# [Nodes Block]
begin: nodes;
structural: structural_node_1,
static,
Px_1, Py_1, Pz_1, #<absolute_position> [m]
3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0, #<absolute_orientation_matrix>
Vx_1, Vy_1, Vz_1, #<absolute_velocity> [m/s]
Wx_1, Wy_1, Wz_1; #<absolute_angular_velocity> [rad/s]
structural: structural_node_2,
dynamic,
Px_2, Py_2, Pz_2, #<absolute_position> [m]
3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0, #<absolute_orientation_matrix>
Vx_2, Vy_2, Vz_2, #<absolute_velocity> [m/s]
Wx_2, Wy_2, Wz_2; #<absolute_angular_velocity> [rad/s]
structural: structural_node_3,
dynamic,
Px_3, Py_3, Pz_3, #<absolute_position> [m]
3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0, #<absolute_orientation_matrix>
Vx_3, Vy_3, Vz_3, #<absolute_velocity> [m/s]
Wx_3, Wy_3, Wz_3; #<absolute_angular_velocity> [rad/s]
structural: structural_node_4,
dynamic,
Px_4, Py_4, Pz_4, #<absolute_position> [m]
3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0, #<absolute_orientation_matrix>
Vx_4, Vy_4, Vz_4, #<absolute_velocity> [m/s]
Wx_4, Wy_4, Wz_4; #<absolute_angular_velocity> [rad/s]
end: nodes;
#-----------------------------------------------------------------------------
# [Elements Block]
begin: elements;
#-----------------------------------------------------------------------------
# [Bodies]
#IMPORTANT NOTE: FreeCAD provides the inertia matrix in the global reference frame,
#while by default, MBDyn assumes it to be in the reference frame of the node,
#thus, the matrix of inertia must be rotated, using the inverse of the placement
#matrix of the node. This is done using the inertial keyword and the following
#orientation matrix.
body: body_2,
structural_node_2, #<node_label>
mass_2, #<mass> [kg]
Rx_2, Ry_2, Rz_2, #<relative_center_of_mass> [m]
Ixx_2, Ixy_2, Ixz_2, #<inertia_matrix> [kg*m^2]
Iyx_2, Iyy_2, Iyz_2,
Izx_2, Izy_2, Izz_2,
orientation, 3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0;
body: body_3,
structural_node_3, #<node_label>
mass_3, #<mass> [kg]
Rx_3, Ry_3, Rz_3, #<relative_center_of_mass> [m]
Ixx_3, Ixy_3, Ixz_3, #<inertia_matrix> [kg*m^2]
Iyx_3, Iyy_3, Iyz_3,
Izx_3, Izy_3, Izz_3,
orientation, 3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0;
body: body_4,
structural_node_4, #<node_label>
mass_4, #<mass> [kg]
Rx_4, Ry_4, Rz_4, #<relative_center_of_mass> [m]
Ixx_4, Ixy_4, Ixz_4, #<inertia_matrix> [kg*m^2]
Iyx_4, Iyy_4, Iyz_4,
Izx_4, Izy_4, Izz_4,
orientation, 3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0;
#-----------------------------------------------------------------------------
# [Joints]
joint: joint_1,
clamp,
structural_node_1, #<node_label>
-0.121, -8.796847998598882e-19, -0.08, #<absolute_pin_position> [m]
3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0; #<absolute_orientation_matrix>
joint: joint_2,
spherical hinge,
structural_node_1, #<node_1_label>
0.0, 0.0, 0.0, #<relative_pin_position_1> [m]
structural_node_2, #<node_2_label>
-0.07, 0.0, -0.055; #<relative_pin_position_2> [m]
joint: joint_3,
revolute hinge,
structural_node_2, #<node_1_label>
0.0, 0.0, 0.0, #<relative_position_1> [m]
orientation, 3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0, #<relative_pin_orientation_matrix_1>
structural_node_3, #<node_2_label>
-0.14, 0.0, -0.024999999999999998, #<relative_position_2> [m]
orientation, 3, 0.0, 0.0, 1.0, 2, guess; #<relative_pin_orientation_matrix_2>
joint: joint_4,
drive hinge,
structural_node_1, #<node_1_label>
orientation, 3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0, #<relative_orientation_matrix_1>
structural_node_2, #<node_2_label>
orientation, 3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0, #<relative_orientation_matrix_2>
single, 0., 0., 1., #<hinge_orientation>
string, "0"; #<hinge_orientation> [rad]
joint: joint_5,
in line,
structural_node_4, #<node_1_label>
0.0, 0.0, 0.0, #<relative_line_position> [m]
3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0, #<relative_orientation>
structural_node_3, #<node_2_label>
offset, 0.14, 0.0, -0.024999999999999998; #<relative_offset> [m]
joint: joint_6,
prismatic,
structural_node_1, #<node_1_label>
orientation, 3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0, #relative_orientation_matrix_1>
structural_node_4, #<node_2_label>
orientation, 3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0; #relative_orientation_matrix_2>
joint: joint_7,
in line,
structural_node_1, #<node_1_label>
0.0, 8.796847998604521e-19, 0.08, #<relative_line_position> [m]
3, 1.0, -2.220446049250313e-16, 2.220446049250313e-16, 2, -2.220446049250313e-16, 0.0, 1.0, #<relative_orientation>
structural_node_4, #<node_2_label>
offset, 0.0, 0.0, 0.0; #<relative_offset> [m]
end: elements;

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1 -0.121 -8.796847998598882e-19 -0.08 1 0 0 0 1 0 0 0 1 -0 -0 0 -0 0 0
2 -0.04869259570202727 -0.001985390890606624 -0.02810879162419694 0.9990678575462876 0.00155825398997522 0.04313916854059252 -1.951563910473908e-18 0.9993482542271943 -0.03609801619284769 -0.04316730264761653 0.03606436769945954 0.9984167192933857 0 -0 -0 0 0 0
3 0.09225341065322781 -0.001895145850124542 -0.009155819605617049 0.9990537652981445 -0.005530477486285024 0.04313916854059253 0.007090681752166232 0.9993230986318842 -0.03609801619284766 -0.04291032831253393 0.03636974511243225 0.9984167192933857 0 0 0 0 0 -0
4 0.2310424585814533 -7.816912863716824e-17 7.816912871471643e-17 1 0 0 0 1 0 0 0 1 0 0 0 0 0 0
1 -0.121 -8.796847998598882e-19 -0.08 1 0 0 0 1 0 0 0 1 -0 -0 0 -0 0 0
2 -0.0486925957020273 -0.001985390890606622 -0.02810879162419696 0.9990678575462876 0.001558253989975216 0.04313916854059258 3.903127820947816e-18 0.9993482542271943 -0.03609801619284767 -0.04316730264761659 0.03606436769945952 0.9984167192933857 0 -0 -0 0 0 0
3 0.0922534106532278 -0.001895145850124542 -0.009155819605617063 0.9990537652981445 -0.005530477486285022 0.04313916854059255 0.007090681752166229 0.9993230986318842 -0.03609801619284766 -0.04291032831253394 0.03636974511243225 0.9984167192933857 0 0 0 0 0 -0
4 0.2310424585814533 -7.816912863716824e-17 7.816912871471643e-17 1 0 0 0 1 0 0 0 1 0 0 0 0 0 0
1 -0.121 -8.796847998598882e-19 -0.08 1 0 0 0 1 0 0 0 1 -0 -0 0 -0 0 0
2 -0.04869259570202728 -0.001985390890606622 -0.02810879162419696 0.9990678575462876 0.001558253989975217 0.04313916854059258 2.168404344971009e-18 0.9993482542271943 -0.03609801619284767 -0.04316730264761659 0.03606436769945952 0.9984167192933857 0 -0 -0 0 0 0
3 0.09225341065322783 -0.001895145850124542 -0.009155819605617063 0.9990537652981445 -0.005530477486285022 0.04313916854059258 0.00709068175216623 0.9993230986318842 -0.03609801619284766 -0.04291032831253397 0.03636974511243225 0.9984167192933857 0 0 0 0 0 -0
4 0.2310424585814533 -7.816912863716824e-17 7.816912871471643e-17 1 0 0 0 1 0 0 0 1 0 0 0 0 0 0
1 -0.121 -8.796847998598882e-19 -0.08 1 0 0 0 1 0 0 0 1 -0 -0 0 -0 0 0
2 -0.04869259570202727 -0.001985390890606624 -0.02810879162419694 0.9990678575462876 0.00155825398997522 0.04313916854059252 -1.951563910473908e-18 0.9993482542271943 -0.03609801619284769 -0.04316730264761653 0.03606436769945954 0.9984167192933857 0 -0 -0 0 0 0
3 0.09225341065322781 -0.001895145850124542 -0.009155819605617049 0.9990537652981445 -0.005530477486285024 0.04313916854059253 0.007090681752166232 0.9993230986318842 -0.03609801619284766 -0.04291032831253393 0.03636974511243225 0.9984167192933857 0 0 0 0 0 -0
4 0.2310424585814533 -7.816912863716824e-17 7.816912871471643e-17 1 0 0 0 1 0 0 0 1 0 0 0 0 0 0
1 -0.121 -8.796847998598882e-19 -0.08 1 0 0 0 1 0 0 0 1 -0 -0 0 -0 0 0
2 -0.0486925957020273 -0.001985390890606622 -0.02810879162419696 0.9990678575462876 0.001558253989975216 0.04313916854059258 3.903127820947816e-18 0.9993482542271943 -0.03609801619284767 -0.04316730264761659 0.03606436769945952 0.9984167192933857 0 -0 -0 0 0 0
3 0.0922534106532278 -0.001895145850124542 -0.009155819605617063 0.9990537652981445 -0.005530477486285022 0.04313916854059255 0.007090681752166229 0.9993230986318842 -0.03609801619284766 -0.04291032831253394 0.03636974511243225 0.9984167192933857 0 0 0 0 0 -0
4 0.2310424585814533 -7.816912863716824e-17 7.816912871471643e-17 1 0 0 0 1 0 0 0 1 0 0 0 0 0 0
1 -0.121 -8.796847998598882e-19 -0.08 1 0 0 0 1 0 0 0 1 -0 -0 0 -0 0 0
2 -0.04869259570202728 -0.001985390890606622 -0.02810879162419696 0.9990678575462876 0.001558253989975217 0.04313916854059258 2.168404344971009e-18 0.9993482542271943 -0.03609801619284767 -0.04316730264761659 0.03606436769945952 0.9984167192933857 0 -0 -0 0 0 0
3 0.09225341065322783 -0.001895145850124542 -0.009155819605617063 0.9990537652981445 -0.005530477486285022 0.04313916854059258 0.00709068175216623 0.9993230986318842 -0.03609801619284766 -0.04291032831253397 0.03636974511243225 0.9984167192933857 0 0 0 0 0 -0
4 0.2310424585814533 -7.816912863716824e-17 7.816912871471643e-17 1 0 0 0 1 0 0 0 1 0 0 0 0 0 0
1 -0.121 -8.796847998598882e-19 -0.08 1 0 0 0 1 0 0 0 1 -0 -0 0 -0 0 0
2 -0.04869259570202727 -0.001985390890606624 -0.02810879162419694 0.9990678575462876 0.00155825398997522 0.04313916854059252 -1.951563910473908e-18 0.9993482542271943 -0.03609801619284769 -0.04316730264761653 0.03606436769945954 0.9984167192933857 0 -0 -0 0 0 0
3 0.09225341065322781 -0.001895145850124542 -0.009155819605617049 0.9990537652981445 -0.005530477486285024 0.04313916854059253 0.007090681752166232 0.9993230986318842 -0.03609801619284766 -0.04291032831253393 0.03636974511243225 0.9984167192933857 0 0 0 0 0 -0
4 0.2310424585814533 -7.816912863716824e-17 7.816912871471643e-17 1 0 0 0 1 0 0 0 1 0 0 0 0 0 0
1 -0.121 -8.796847998598882e-19 -0.08 1 0 0 0 1 0 0 0 1 -0 -0 0 -0 0 0
2 -0.0486925957020273 -0.001985390890606622 -0.02810879162419696 0.9990678575462876 0.001558253989975216 0.04313916854059258 3.903127820947816e-18 0.9993482542271943 -0.03609801619284767 -0.04316730264761659 0.03606436769945952 0.9984167192933857 0 -0 -0 0 0 0
3 0.0922534106532278 -0.001895145850124542 -0.009155819605617063 0.9990537652981445 -0.005530477486285022 0.04313916854059255 0.007090681752166229 0.9993230986318842 -0.03609801619284766 -0.04291032831253394 0.03636974511243225 0.9984167192933857 0 0 0 0 0 -0
4 0.2310424585814533 -7.816912863716824e-17 7.816912871471643e-17 1 0 0 0 1 0 0 0 1 0 0 0 0 0 0
1 -0.121 -8.796847998598882e-19 -0.08 1 0 0 0 1 0 0 0 1 -0 -0 0 -0 0 0
2 -0.04869259570202728 -0.001985390890606622 -0.02810879162419696 0.9990678575462876 0.001558253989975217 0.04313916854059258 2.168404344971009e-18 0.9993482542271943 -0.03609801619284767 -0.04316730264761659 0.03606436769945952 0.9984167192933857 0 -0 -0 0 0 0
3 0.09225341065322783 -0.001895145850124542 -0.009155819605617063 0.9990537652981445 -0.005530477486285022 0.04313916854059258 0.00709068175216623 0.9993230986318842 -0.03609801619284766 -0.04291032831253397 0.03636974511243225 0.9984167192933857 0 0 0 0 0 -0
4 0.2310424585814533 -7.816912863716824e-17 7.816912871471643e-17 1 0 0 0 1 0 0 0 1 0 0 0 0 0 0
1 -0.121 -8.796847998598882e-19 -0.08 1 0 0 0 1 0 0 0 1 -0 -0 0 -0 0 0
2 -0.04869259570202727 -0.001985390890606624 -0.02810879162419694 0.9990678575462876 0.00155825398997522 0.04313916854059252 -1.951563910473908e-18 0.9993482542271943 -0.03609801619284769 -0.04316730264761653 0.03606436769945954 0.9984167192933857 0 -0 -0 0 0 0
3 0.09225341065322781 -0.001895145850124542 -0.009155819605617049 0.9990537652981445 -0.005530477486285024 0.04313916854059253 0.007090681752166232 0.9993230986318842 -0.03609801619284766 -0.04291032831253393 0.03636974511243225 0.9984167192933857 0 0 0 0 0 -0
4 0.2310424585814533 -7.816912863716824e-17 7.816912871471643e-17 1 0 0 0 1 0 0 0 1 0 0 0 0 0 0
1 -0.121 -8.796847998598882e-19 -0.08 1 0 0 0 1 0 0 0 1 -0 -0 0 -0 0 0
2 -0.0486925957020273 -0.001985390890606622 -0.02810879162419696 0.9990678575462876 0.001558253989975216 0.04313916854059258 3.903127820947816e-18 0.9993482542271943 -0.03609801619284767 -0.04316730264761659 0.03606436769945952 0.9984167192933857 0 -0 -0 0 0 0
3 0.0922534106532278 -0.001895145850124542 -0.009155819605617063 0.9990537652981445 -0.005530477486285022 0.04313916854059255 0.007090681752166229 0.9993230986318842 -0.03609801619284766 -0.04291032831253394 0.03636974511243225 0.9984167192933857 0 0 0 0 0 -0
4 0.2310424585814533 -7.816912863716824e-17 7.816912871471643e-17 1 0 0 0 1 0 0 0 1 0 0 0 0 0 0
1 -0.121 -8.796847998598882e-19 -0.08 1 0 0 0 1 0 0 0 1 -0 -0 0 -0 0 0
2 -0.04869259570202728 -0.001985390890606622 -0.02810879162419696 0.9990678575462876 0.001558253989975217 0.04313916854059258 2.168404344971009e-18 0.9993482542271943 -0.03609801619284767 -0.04316730264761659 0.03606436769945952 0.9984167192933857 0 -0 -0 0 0 0
3 0.09225341065322783 -0.001895145850124542 -0.009155819605617063 0.9990537652981445 -0.005530477486285022 0.04313916854059258 0.00709068175216623 0.9993230986318842 -0.03609801619284766 -0.04291032831253397 0.03636974511243225 0.9984167192933857 0 0 0 0 0 -0
4 0.2310424585814533 -7.816912863716824e-17 7.816912871471643e-17 1 0 0 0 1 0 0 0 1 0 0 0 0 0 0
1 -0.121 -8.796847998598882e-19 -0.08 1 0 0 0 1 0 0 0 1 -0 -0 0 -0 0 0
2 -0.04869259570202727 -0.001985390890606624 -0.02810879162419694 0.9990678575462876 0.00155825398997522 0.04313916854059252 -1.951563910473908e-18 0.9993482542271943 -0.03609801619284769 -0.04316730264761653 0.03606436769945954 0.9984167192933857 0 -0 -0 0 0 0
3 0.09225341065322781 -0.001895145850124542 -0.009155819605617049 0.9990537652981445 -0.005530477486285024 0.04313916854059253 0.007090681752166232 0.9993230986318842 -0.03609801619284766 -0.04291032831253393 0.03636974511243225 0.9984167192933857 0 0 0 0 0 -0
4 0.2310424585814533 -7.816912863716824e-17 7.816912871471643e-17 1 0 0 0 1 0 0 0 1 0 0 0 0 0 0
1 -0.121 -8.796847998598882e-19 -0.08 1 0 0 0 1 0 0 0 1 -0 -0 0 -0 0 0
2 -0.0486925957020273 -0.001985390890606622 -0.02810879162419696 0.9990678575462876 0.001558253989975216 0.04313916854059258 3.903127820947816e-18 0.9993482542271943 -0.03609801619284767 -0.04316730264761659 0.03606436769945952 0.9984167192933857 0 -0 -0 0 0 0
3 0.0922534106532278 -0.001895145850124542 -0.009155819605617063 0.9990537652981445 -0.005530477486285022 0.04313916854059255 0.007090681752166229 0.9993230986318842 -0.03609801619284766 -0.04291032831253394 0.03636974511243225 0.9984167192933857 0 0 0 0 0 -0
4 0.2310424585814533 -7.816912863716824e-17 7.816912871471643e-17 1 0 0 0 1 0 0 0 1 0 0 0 0 0 0
1 -0.121 -8.796847998598882e-19 -0.08 1 0 0 0 1 0 0 0 1 -0 -0 0 -0 0 0
2 -0.04869259570202728 -0.001985390890606622 -0.02810879162419696 0.9990678575462876 0.001558253989975217 0.04313916854059258 2.168404344971009e-18 0.9993482542271943 -0.03609801619284767 -0.04316730264761659 0.03606436769945952 0.9984167192933857 0 -0 -0 0 0 0
3 0.09225341065322783 -0.001895145850124542 -0.009155819605617063 0.9990537652981445 -0.005530477486285022 0.04313916854059258 0.00709068175216623 0.9993230986318842 -0.03609801619284766 -0.04291032831253397 0.03636974511243225 0.9984167192933857 0 0 0 0 0 -0
4 0.2310424585814533 -7.816912863716824e-17 7.816912871471643e-17 1 0 0 0 1 0 0 0 1 0 0 0 0 0 0
1 -0.121 -8.796847998598882e-19 -0.08 1 0 0 0 1 0 0 0 1 -0 -0 0 -0 0 0
2 -0.04869259570202727 -0.001985390890606624 -0.02810879162419694 0.9990678575462876 0.00155825398997522 0.04313916854059252 -1.951563910473908e-18 0.9993482542271943 -0.03609801619284769 -0.04316730264761653 0.03606436769945954 0.9984167192933857 0 -0 -0 0 0 0
3 0.09225341065322781 -0.001895145850124542 -0.009155819605617049 0.9990537652981445 -0.005530477486285024 0.04313916854059253 0.007090681752166232 0.9993230986318842 -0.03609801619284766 -0.04291032831253393 0.03636974511243225 0.9984167192933857 0 0 0 0 0 -0
4 0.2310424585814533 -7.816912863716824e-17 7.816912871471643e-17 1 0 0 0 1 0 0 0 1 0 0 0 0 0 0
1 -0.121 -8.796847998598882e-19 -0.08 1 0 0 0 1 0 0 0 1 -0 -0 0 -0 0 0
2 -0.0486925957020273 -0.001985390890606622 -0.02810879162419696 0.9990678575462876 0.001558253989975216 0.04313916854059258 3.903127820947816e-18 0.9993482542271943 -0.03609801619284767 -0.04316730264761659 0.03606436769945952 0.9984167192933857 0 -0 -0 0 0 0
3 0.0922534106532278 -0.001895145850124542 -0.009155819605617063 0.9990537652981445 -0.005530477486285022 0.04313916854059255 0.007090681752166229 0.9993230986318842 -0.03609801619284766 -0.04291032831253394 0.03636974511243225 0.9984167192933857 0 0 0 0 0 -0
4 0.2310424585814533 -7.816912863716824e-17 7.816912871471643e-17 1 0 0 0 1 0 0 0 1 0 0 0 0 0 0

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#-----------------------------------------------------------------------------
# [Data Block]
begin: data;
problem: initial value;
end: data;
#-----------------------------------------------------------------------------
# [Problem Block]
begin: initial value;
initial time: 0.0;
final time: 3.0;
time step: 0.01;
max iterations: 100;
tolerance: 1e-06;
derivatives tolerance: 0.0001;
derivatives max iterations: 100;
derivatives coefficient: auto;
end: initial value;
#-----------------------------------------------------------------------------
# [Control Data Block]
begin: control data;
max iterations: 1000;
default orientation: euler321;
omega rotates: no;
print: none;
initial stiffness: 1.0, 1.0;
structural nodes: 4;
rigid bodies: 3;
joints: 6;
end: control data;
#-----------------------------------------------------------------------------
# [Design Variables]
#Generic bodies
#body: 2
set: integer body_2 = 2; #body label
set: real mass_2 = 1.448636188351172; #mass [kg]
set: real volume_2 = 0.00018337166941154076; #volume [m^3]
#body: 3
set: integer body_3 = 3; #body label
set: real mass_3 = 2.8529486557067685; #mass [kg]
set: real volume_3 = 0.0003611327412287049; #volume [m^3]
#body: 4
set: integer body_4 = 4; #body label
set: real mass_4 = 10.859427202622141; #mass [kg]
set: real volume_4 = 0.0013746110383066003; #volume [m^3]
#Nodes
#node: 1
set: integer structural_node_1 = 1; #node label
#node: 2
set: integer structural_node_2 = 2; #node label
#node: 3
set: integer structural_node_3 = 3; #node label
#node: 4
set: integer structural_node_4 = 4; #node label
#Joints
#joint: 1
set: integer joint_1 = 1; #joint label
#joint: 2
set: integer joint_2 = 2; #joint label
#joint: 3
set: integer joint_3 = 3; #joint label
#joint: 4
set: integer joint_4 = 4; #joint label
#joint: 5
set: integer joint_5 = 5; #joint label
#joint: 6
set: integer joint_6 = 6; #joint label
#Nodes: initial conditions
#node: 1
set: real Px_1 = -0.121; #X component of the absolute position [m]
set: real Py_1 = -1.218180697837851e-18; #Y component of the absolute position [m]
set: real Pz_1 = -0.08; #Z component of the absolute position [m]
set: real Vx_1 = 0.0; #X component of the absolute velocity [m/s]
set: real Vy_1 = 0.0; #Y component of the absolute velocity [m/s]
set: real Vz_1 = 0.0; #Z component of the absolute velocity [m/s]
set: real Wx_1 = 0.0; #X component of the absolute angular velocity [rad/s]
set: real Wy_1 = 0.0; #Y component of the absolute angular velocity [rad/s]
set: real Wz_1 = 0.0; #Z component of the absolute angular velocity [rad/s]
#node: 2
set: real Px_2 = -0.047537048944738425; #X component of the absolute position [m]
set: real Py_2 = 0.09742200410568831; #Y component of the absolute position [m]
set: real Pz_2 = -0.030293476812230588; #Z component of the absolute position [m]
set: real Vx_2 = 0.0; #X component of the absolute velocity [m/s]
set: real Vy_2 = 0.0; #Y component of the absolute velocity [m/s]
set: real Vz_2 = 0.0; #Z component of the absolute velocity [m/s]
set: real Wx_2 = 0.0; #X component of the absolute angular velocity [rad/s]
set: real Wy_2 = 0.0; #Y component of the absolute angular velocity [rad/s]
set: real Wz_2 = 0.0; #Z component of the absolute angular velocity [rad/s]
#node: 3
set: real Px_3 = 0.07099630277370235; #X component of the absolute position [m]
set: real Py_3 = -0.07364765799707981; #Y component of the absolute position [m]
set: real Pz_3 = 0.058407900823760565; #Z component of the absolute position [m]
set: real Vx_3 = 0.0; #X component of the absolute velocity [m/s]
set: real Vy_3 = 0.0; #Y component of the absolute velocity [m/s]
set: real Vz_3 = 0.0; #Z component of the absolute velocity [m/s]
set: real Wx_3 = 0.0; #X component of the absolute angular velocity [rad/s]
set: real Wy_3 = 0.0; #Y component of the absolute angular velocity [rad/s]
set: real Wz_3 = 0.0; #Z component of the absolute angular velocity [rad/s]
#node: 4
set: real Px_4 = 0.3723079639890564; #X component of the absolute position [m]
set: real Py_4 = 0.04333150035096042; #Y component of the absolute position [m]
set: real Pz_4 = 0.008140985321785409; #Z component of the absolute position [m]
set: real Vx_4 = 0.0; #X component of the absolute velocity [m/s]
set: real Vy_4 = 0.0; #Y component of the absolute velocity [m/s]
set: real Vz_4 = 0.0; #Z component of the absolute velocity [m/s]
set: real Wx_4 = 0.0; #X component of the absolute angular velocity [rad/s]
set: real Wy_4 = 0.0; #Y component of the absolute angular velocity [rad/s]
set: real Wz_4 = 0.0; #Z component of the absolute angular velocity [rad/s]
#-----------------------------------------------------------------------------
# [Intermediate Variables]
#Moments of inertia and relative center of mass
#body 2:
set: real Ixx_2 = 0.0028717510150880004; #moment of inertia [kg*m^2]
set: real Iyy_2 = 0.002864447840812; #moment of inertia [kg*m^2]
set: real Izz_2 = 0.0007089594589930001; #moment of inertia [kg*m^2]
set: real Rx_2 = 7.105427357601002e-18; #X component of the relative center of mass [m]
set: real Ry_2 = 0.0; #Y component of the relative center of mass [m]
set: real Rz_2 = 7.105427357601002e-18; #Z component of the relative center of mass [m]
#body 3:
set: real Ixx_3 = 0.033837921987970004; #moment of inertia [kg*m^2]
set: real Iyy_3 = 0.033715148099504; #moment of inertia [kg*m^2]
set: real Izz_3 = 0.001956310318013; #moment of inertia [kg*m^2]
set: real Rx_3 = 2.842170943040401e-17; #X component of the relative center of mass [m]
set: real Ry_3 = -1.4210854715202004e-17; #Y component of the relative center of mass [m]
set: real Rz_3 = 0.0; #Z component of the relative center of mass [m]
#body 4:
set: real Ixx_4 = 0.07706742098794901; #moment of inertia [kg*m^2]
set: real Iyy_4 = 0.066351815798527; #moment of inertia [kg*m^2]
set: real Izz_4 = 0.061792350456255; #moment of inertia [kg*m^2]
set: real Rx_4 = 2.842170943040401e-16; #X component of the relative center of mass [m]
set: real Ry_4 = 2.1316282072803006e-17; #Y component of the relative center of mass [m]
set: real Rz_4 = 2.2737367544323206e-16; #Z component of the relative center of mass [m]
#-----------------------------------------------------------------------------
# [Nodes Block]
begin: nodes;
structural: structural_node_1,
static,
Px_1, Py_1, Pz_1, #<absolute_position> [m]
3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0, #<absolute_orientation_matrix>
Vx_1, Vy_1, Vz_1, #<absolute_velocity> [m/s]
Wx_1, Wy_1, Wz_1; #<absolute_angular_velocity> [rad/s]
structural: structural_node_2,
dynamic,
Px_2, Py_2, Pz_2, #<absolute_position> [m]
3, 0.28116838555915347, -0.12674940821214617, 0.9512512425641977, 2, -0.12674940821214617, 0.9776506595433675, 0.16773125949652098, #<absolute_orientation_matrix>
Vx_2, Vy_2, Vz_2, #<absolute_velocity> [m/s]
Wx_2, Wy_2, Wz_2; #<absolute_angular_velocity> [rad/s]
structural: structural_node_3,
dynamic,
Px_3, Py_3, Pz_3, #<absolute_position> [m]
3, -0.27178893568691503, -0.25783416049630004, 0.9271743741709766, 2, 0.014330116918634624, 0.9622501868990581, 0.271788935686915, #<absolute_orientation_matrix>
Vx_3, Vy_3, Vz_3, #<absolute_velocity> [m/s]
Wx_3, Wy_3, Wz_3; #<absolute_angular_velocity> [rad/s]
structural: structural_node_4,
dynamic,
Px_4, Py_4, Pz_4, #<absolute_position> [m]
3, 0.2588190451025211, 0.0, 0.9659258262890682, 2, 0.0, 1.0, 0.0, #<absolute_orientation_matrix>
Vx_4, Vy_4, Vz_4, #<absolute_velocity> [m/s]
Wx_4, Wy_4, Wz_4; #<absolute_angular_velocity> [rad/s]
end: nodes;
#-----------------------------------------------------------------------------
# [Elements Block]
begin: elements;
#-----------------------------------------------------------------------------
# [Bodies]
body: body_2,
structural_node_2, #<node_label>
mass_2, #<mass> [kg]
Rx_2, Ry_2, Rz_2, #<relative_center_of_mass> [m]
diag, Ixx_2, Iyy_2, Izz_2, #<inertia matrix> [kg*m^2]
orientation, 3, -0.0054384608129255385, 0.8559103374577453, 0.5150405937686557, 2, 0.9969290667160357, -0.0024978913689130133, 0.0023196850194898005;
body: body_3,
structural_node_3, #<node_label>
mass_3, #<mass> [kg]
Rx_3, Ry_3, Rz_3, #<relative_center_of_mass> [m]
diag, Ixx_3, Iyy_3, Izz_3, #<inertia matrix> [kg*m^2]
orientation, 3, 0.9973238325492868, 0.0012847690482160057, -0.002629529780301787, 2, -0.00011328308715380375, 1.0027304733964244, 0.004450235157436283;
body: body_4,
structural_node_4, #<node_label>
mass_4, #<mass> [kg]
Rx_4, Ry_4, Rz_4, #<relative_center_of_mass> [m]
diag, Ixx_4, Iyy_4, Izz_4, #<inertia matrix> [kg*m^2]
orientation, 3, -8.551421488581235e-05, 0.0, 0.9957768995806164, 2, 0.0, 1.0, 0.0;
#-----------------------------------------------------------------------------
# [Joints]
joint: joint_1,
clamp,
structural_node_1, #<node_label>
-0.121, -1.218180697837851e-18, -0.08, #<absolute_pin_position> [m]
3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0; #<absolute_orientation_matrix>
joint: joint_2,
axial rotation,
structural_node_1, #<node_1_label>
0.0, 1.218180697837851e-18, 0.05, #<relative_offset_1> [m]
orientation, 3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0, #<relative_orientation_matrix_1>
structural_node_2, #<node_2_label>
-0.03739853284269051, 0.0, 0.0032867622552210634, #<relative_offset_2> [m]
orientation, 3, 5.204170427930421e-18, 0.0, 1.0, 2, guess, #<relative_orientation_matrix_2>
string, "model::drive(1, Time)"; #<angular_velocity> [rad/s]
joint: joint_3,
revolute hinge,
structural_node_2, #<node_1_label>
0.03260146715730949, 1.4210854715202004e-17, 0.05328676225522106, #<relative_position_1> [m]
orientation, 3, 5.204170427930421e-18, 0.0, 1.0, 2, 0.0, 1.0, 0.0, #<relative_pin_orientation_matrix_1>
structural_node_3, #<node_2_label>
-0.1400000000000079, -1.0444978215673472e-15, 0.024999999999998038, #<relative_position_2> [m]
orientation, 3, -5.551115123125784e-17, -5.984795992119986e-17, 1.0, 2, guess; #<relative_pin_orientation_matrix_2>
joint: joint_4,
in line,
structural_node_3, #<node_1_label>
0.13999999999999133, 4.4231285301066236e-16, 9.79127889877418e-15, #<relative_line_position> [m]
3, 2.7195091690402506e-15, 1.2586758486779817e-14, 1.0, 2, 0.6882367162699149, 0.7254861972346578, -1.1003185610451133e-14, #<relative_orientation>
structural_node_4, #<node_2_label>
offset, -0.045580834634119244, -2.0299354019925886e-10, 1.2562251640702015e-08; #<relative_offset> [m]
joint: joint_5,
in line,
structural_node_1, #<node_1_label>
0.0, 1.2181806978377854e-18, 0.08, #<relative_line_position> [m]
3, 1.0, -2.220446049250313e-16, 2.220446049250313e-16, 2, -2.220446049250313e-16, 0.0, 1.0, #<relative_orientation>
structural_node_4, #<node_2_label>
offset, -0.045580834634119244, -2.0299354019925886e-10, 1.2562251640702015e-08; #<relative_offset> [m]
joint: joint_6,
prismatic,
structural_node_1, #<node_1_label>
orientation, 3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0, #relative_orientation_matrix_1>
structural_node_4, #<node_2_label>
orientation, 3, 0, 0, 1, 2, 0, 1, 0; #relative_orientation_matrix_2>
#-----------------------------------------------------------------------------
# [Drive callers]
drive caller: 1, name,"drive:1", ramp, 6.28, 0.0, 1.0, 0.0;
end: elements;

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#-----------------------------------------------------------------------------
# [Data Block]
begin: data;
problem: initial value;
end: data;
#-----------------------------------------------------------------------------
# [Problem Block]
begin: initial value;
initial time: 0.0;
final time: 8.0;
time step: 0.01;
max iterations: 100;
tolerance: 1e-06;
derivatives tolerance: 0.0001;
derivatives max iterations: 100;
derivatives coefficient: auto;
end: initial value;
#-----------------------------------------------------------------------------
# [Control Data Block]
begin: control data;
max iterations: 1000;
default orientation: euler321;
omega rotates: no;
print: none;
initial stiffness: 1.0, 1.0;
structural nodes: 4;
rigid bodies: 3;
joints: 6;
end: control data;
#-----------------------------------------------------------------------------
# [Design Variables]
#Generic bodies
#body: 2
set: integer body_2 = 2; #body label
set: real mass_2 = 1.448636188351172; #mass [kg]
set: real volume_2 = 0.00018337166941154076; #volume [m^3]
#body: 3
set: integer body_3 = 3; #body label
set: real mass_3 = 2.8529486557067685; #mass [kg]
set: real volume_3 = 0.0003611327412287049; #volume [m^3]
#body: 4
set: integer body_4 = 4; #body label
set: real mass_4 = 10.859427202622141; #mass [kg]
set: real volume_4 = 0.0013746110383066003; #volume [m^3]
#Nodes
#node: 1
set: integer structural_node_1 = 1; #node label
#node: 2
set: integer structural_node_2 = 2; #node label
#node: 3
set: integer structural_node_3 = 3; #node label
#node: 4
set: integer structural_node_4 = 4; #node label
#Joints
#joint: 1
set: integer joint_1 = 1; #joint label
#joint: 2
set: integer joint_2 = 2; #joint label
#joint: 3
set: integer joint_3 = 3; #joint label
#joint: 4
set: integer joint_4 = 4; #joint label
#joint: 5
set: integer joint_5 = 5; #joint label
#joint: 6
set: integer joint_6 = 6; #joint label
#Nodes: initial conditions
#node: 1
set: real Px_1 = -0.121; #X component of the absolute position [m]
set: real Py_1 = -1.218180697837851e-18; #Y component of the absolute position [m]
set: real Pz_1 = -0.08; #Z component of the absolute position [m]
set: real Vx_1 = 0.0; #X component of the absolute velocity [m/s]
set: real Vy_1 = 0.0; #Y component of the absolute velocity [m/s]
set: real Vz_1 = 0.0; #Z component of the absolute velocity [m/s]
set: real Wx_1 = 0.0; #X component of the absolute angular velocity [rad/s]
set: real Wy_1 = 0.0; #Y component of the absolute angular velocity [rad/s]
set: real Wz_1 = 0.0; #Z component of the absolute angular velocity [rad/s]
#node: 2
set: real Px_2 = -0.047537048944738425; #X component of the absolute position [m]
set: real Py_2 = 0.09742200410568831; #Y component of the absolute position [m]
set: real Pz_2 = -0.030293476812230588; #Z component of the absolute position [m]
set: real Vx_2 = 0.0; #X component of the absolute velocity [m/s]
set: real Vy_2 = 0.0; #Y component of the absolute velocity [m/s]
set: real Vz_2 = 0.0; #Z component of the absolute velocity [m/s]
set: real Wx_2 = 0.0; #X component of the absolute angular velocity [rad/s]
set: real Wy_2 = 0.0; #Y component of the absolute angular velocity [rad/s]
set: real Wz_2 = 0.0; #Z component of the absolute angular velocity [rad/s]
#node: 3
set: real Px_3 = 0.07099630277370235; #X component of the absolute position [m]
set: real Py_3 = -0.07364765799707981; #Y component of the absolute position [m]
set: real Pz_3 = 0.058407900823760565; #Z component of the absolute position [m]
set: real Vx_3 = 0.0; #X component of the absolute velocity [m/s]
set: real Vy_3 = 0.0; #Y component of the absolute velocity [m/s]
set: real Vz_3 = 0.0; #Z component of the absolute velocity [m/s]
set: real Wx_3 = 0.0; #X component of the absolute angular velocity [rad/s]
set: real Wy_3 = 0.0; #Y component of the absolute angular velocity [rad/s]
set: real Wz_3 = 0.0; #Z component of the absolute angular velocity [rad/s]
#node: 4
set: real Px_4 = 0.3723079639890564; #X component of the absolute position [m]
set: real Py_4 = 0.04333150035096042; #Y component of the absolute position [m]
set: real Pz_4 = 0.008140985321785409; #Z component of the absolute position [m]
set: real Vx_4 = 0.0; #X component of the absolute velocity [m/s]
set: real Vy_4 = 0.0; #Y component of the absolute velocity [m/s]
set: real Vz_4 = 0.0; #Z component of the absolute velocity [m/s]
set: real Wx_4 = 0.0; #X component of the absolute angular velocity [rad/s]
set: real Wy_4 = 0.0; #Y component of the absolute angular velocity [rad/s]
set: real Wz_4 = 0.0; #Z component of the absolute angular velocity [rad/s]
#-----------------------------------------------------------------------------
# [Intermediate Variables]
#Moments of inertia and relative center of mass
#body 2:
set: real Ixx_2 = 0.0028717510150880004; #moment of inertia [kg*m^2]
set: real Iyy_2 = 0.002864447840812; #moment of inertia [kg*m^2]
set: real Izz_2 = 0.0007089594589930001; #moment of inertia [kg*m^2]
set: real Rx_2 = 7.105427357601002e-18; #X component of the relative center of mass [m]
set: real Ry_2 = 0.0; #Y component of the relative center of mass [m]
set: real Rz_2 = 7.105427357601002e-18; #Z component of the relative center of mass [m]
#body 3:
set: real Ixx_3 = 0.033837921987970004; #moment of inertia [kg*m^2]
set: real Iyy_3 = 0.033715148099504; #moment of inertia [kg*m^2]
set: real Izz_3 = 0.001956310318013; #moment of inertia [kg*m^2]
set: real Rx_3 = 2.842170943040401e-17; #X component of the relative center of mass [m]
set: real Ry_3 = -1.4210854715202004e-17; #Y component of the relative center of mass [m]
set: real Rz_3 = 0.0; #Z component of the relative center of mass [m]
#body 4:
set: real Ixx_4 = 0.07706742098794901; #moment of inertia [kg*m^2]
set: real Iyy_4 = 0.066351815798527; #moment of inertia [kg*m^2]
set: real Izz_4 = 0.061792350456255; #moment of inertia [kg*m^2]
set: real Rx_4 = 2.842170943040401e-16; #X component of the relative center of mass [m]
set: real Ry_4 = 2.1316282072803006e-17; #Y component of the relative center of mass [m]
set: real Rz_4 = 2.2737367544323206e-16; #Z component of the relative center of mass [m]
#-----------------------------------------------------------------------------
# [Nodes Block]
begin: nodes;
structural: structural_node_1,
static,
Px_1, Py_1, Pz_1, #<absolute_position> [m]
3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0, #<absolute_orientation_matrix>
Vx_1, Vy_1, Vz_1, #<absolute_velocity> [m/s]
Wx_1, Wy_1, Wz_1; #<absolute_angular_velocity> [rad/s]
structural: structural_node_2,
dynamic,
Px_2, Py_2, Pz_2, #<absolute_position> [m]
3, 0.28116838555915347, -0.12674940821214617, 0.9512512425641977, 2, -0.12674940821214617, 0.9776506595433675, 0.16773125949652098, #<absolute_orientation_matrix>
Vx_2, Vy_2, Vz_2, #<absolute_velocity> [m/s]
Wx_2, Wy_2, Wz_2; #<absolute_angular_velocity> [rad/s]
structural: structural_node_3,
dynamic,
Px_3, Py_3, Pz_3, #<absolute_position> [m]
3, -0.27178893568691503, -0.25783416049630004, 0.9271743741709766, 2, 0.014330116918634624, 0.9622501868990581, 0.271788935686915, #<absolute_orientation_matrix>
Vx_3, Vy_3, Vz_3, #<absolute_velocity> [m/s]
Wx_3, Wy_3, Wz_3; #<absolute_angular_velocity> [rad/s]
structural: structural_node_4,
dynamic,
Px_4, Py_4, Pz_4, #<absolute_position> [m]
3, 0.2588190451025211, 0.0, 0.9659258262890682, 2, 0.0, 1.0, 0.0, #<absolute_orientation_matrix>
Vx_4, Vy_4, Vz_4, #<absolute_velocity> [m/s]
Wx_4, Wy_4, Wz_4; #<absolute_angular_velocity> [rad/s]
end: nodes;
#-----------------------------------------------------------------------------
# [Elements Block]
begin: elements;
#-----------------------------------------------------------------------------
# [Bodies]
body: body_2,
structural_node_2, #<node_label>
mass_2, #<mass> [kg]
Rx_2, Ry_2, Rz_2, #<relative_center_of_mass> [m]
diag, Ixx_2, Iyy_2, Izz_2, #<inertia matrix> [kg*m^2]
orientation, 3, -0.0054384608129255385, 0.8559103374577453, 0.5150405937686557, 2, 0.9969290667160357, -0.0024978913689130133, 0.0023196850194898005;
body: body_3,
structural_node_3, #<node_label>
mass_3, #<mass> [kg]
Rx_3, Ry_3, Rz_3, #<relative_center_of_mass> [m]
diag, Ixx_3, Iyy_3, Izz_3, #<inertia matrix> [kg*m^2]
orientation, 3, 0.9973238325492868, 0.0012847690482160057, -0.002629529780301787, 2, -0.00011328308715380375, 1.0027304733964244, 0.004450235157436283;
body: body_4,
structural_node_4, #<node_label>
mass_4, #<mass> [kg]
Rx_4, Ry_4, Rz_4, #<relative_center_of_mass> [m]
diag, Ixx_4, Iyy_4, Izz_4, #<inertia matrix> [kg*m^2]
orientation, 3, -8.551421488581235e-05, 0.0, 0.9957768995806164, 2, 0.0, 1.0, 0.0;
#-----------------------------------------------------------------------------
# [Joints]
joint: joint_1,
clamp,
structural_node_1, #<node_label>
-0.121, -1.218180697837851e-18, -0.08, #<absolute_pin_position> [m]
3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0; #<absolute_orientation_matrix>
joint: joint_2,
axial rotation,
structural_node_1, #<node_1_label>
0.0, 1.218180697837851e-18, 0.05, #<relative_offset_1> [m]
orientation, 3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0, #<relative_orientation_matrix_1>
structural_node_2, #<node_2_label>
-0.03739853284269051, 0.0, 0.0032867622552210634, #<relative_offset_2> [m]
orientation, 3, 5.204170427930421e-18, 0.0, 1.0, 2, guess, #<relative_orientation_matrix_2>
string, "model::drive(1, Time)"; #<angular_velocity> [rad/s]
joint: joint_3,
revolute hinge,
structural_node_2, #<node_1_label>
0.03260146715730949, 1.4210854715202004e-17, 0.05328676225522106, #<relative_position_1> [m]
orientation, 3, 5.204170427930421e-18, 0.0, 1.0, 2, 0.0, 1.0, 0.0, #<relative_pin_orientation_matrix_1>
structural_node_3, #<node_2_label>
-0.1400000000000079, -1.0444978215673472e-15, 0.024999999999998038, #<relative_position_2> [m]
orientation, 3, -5.551115123125784e-17, -5.984795992119986e-17, 1.0, 2, guess; #<relative_pin_orientation_matrix_2>
joint: joint_4,
in line,
structural_node_3, #<node_1_label>
0.13999999999999133, 4.4231285301066236e-16, 9.79127889877418e-15, #<relative_line_position> [m]
3, 2.7195091690402506e-15, 1.2586758486779817e-14, 1.0, 2, 0.6882367162699149, 0.7254861972346578, -1.1003185610451133e-14, #<relative_orientation>
structural_node_4, #<node_2_label>
offset, -0.045580834634119244, -2.0299354019925886e-10, 1.2562251640702015e-08; #<relative_offset> [m]
joint: joint_5,
in line,
structural_node_1, #<node_1_label>
0.0, 1.2181806978377854e-18, 0.08, #<relative_line_position> [m]
3, 1.0, -2.220446049250313e-16, 2.220446049250313e-16, 2, -2.220446049250313e-16, 0.0, 1.0, #<relative_orientation>
structural_node_4, #<node_2_label>
offset, -0.045580834634119244, -2.0299354019925886e-10, 1.2562251640702015e-08; #<relative_offset> [m]
joint: joint_6,
prismatic,
structural_node_1, #<node_1_label>
orientation, 3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0, #relative_orientation_matrix_1>
structural_node_4, #<node_2_label>
orientation, 3, 0, 0, 1, 2, 0, 1, 0; #relative_orientation_matrix_2>
#-----------------------------------------------------------------------------
# [Drive callers]
drive caller: 1, name,"drive:1", ramp, 6.28, 0.0, 1.0, 0.0;
end: elements;

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#-----------------------------------------------------------------------------
# [Data Block]
begin: data;
problem: initial value;
end: data;
#-----------------------------------------------------------------------------
# [Problem Block]
begin: initial value;
initial time: 0.0;
final time: 8.0;
time step: 0.01;
max iterations: 100;
tolerance: 1e-06;
derivatives tolerance: 0.0001;
derivatives max iterations: 100;
derivatives coefficient: auto;
end: initial value;
#-----------------------------------------------------------------------------
# [Control Data Block]
begin: control data;
max iterations: 1000;
default orientation: orientation matrix;
omega rotates: no;
print: none;
initial stiffness: 1.0, 1.0;
structural nodes: 5;
rigid bodies: 3;
joints: 6;
end: control data;
#-----------------------------------------------------------------------------
# [Design Variables]
#Generic bodies
#body: 2
set: integer body_2 = 2; #body label
set: real mass_2 = 0.24147734685710437; #mass [kg]
set: real volume_2 = 3.056675276672207e-05; #volume [m^3]
#body: 4
set: integer body_4 = 4; #body label
set: real mass_4 = 0.11253654770310718; #mass [kg]
set: real volume_4 = 1.4245132620646478e-05; #volume [m^3]
#body: 5
set: integer body_5 = 5; #body label
set: real mass_5 = 0.11253654770310723; #mass [kg]
set: real volume_5 = 1.4245132620646483e-05; #volume [m^3]
#Nodes
#node: 1
set: integer structural_node_1 = 1; #node label
#node: 2
set: integer structural_node_2 = 2; #node label
#node: 3
set: integer structural_node_3 = 3; #node label
#node: 4
set: integer structural_node_4 = 4; #node label
#node: 5
set: integer structural_node_5 = 5; #node label
#Joints
#joint: 1
set: integer joint_1 = 1; #joint label
#joint: 2
set: integer joint_2 = 2; #joint label
#joint: 3
set: integer joint_3 = 3; #joint label
#joint: 4
set: integer joint_4 = 4; #joint label
#joint: 5
set: integer joint_5 = 5; #joint label
#joint: 7
set: integer joint_7 = 7; #joint label
#Nodes: initial conditions
#node: 1
set: real Px_1 = 0.16912189837562464; #X component of the absolute position [m]
set: real Py_1 = -0.10055206743263254; #Y component of the absolute position [m]
set: real Pz_1 = 0.07867737409397452; #Z component of the absolute position [m]
set: real Vx_1 = 0.0; #X component of the absolute velocity [m/s]
set: real Vy_1 = 0.0; #Y component of the absolute velocity [m/s]
set: real Vz_1 = 0.0; #Z component of the absolute velocity [m/s]
set: real Wx_1 = 0.0; #X component of the absolute angular velocity [rad/s]
set: real Wy_1 = 0.0; #Y component of the absolute angular velocity [rad/s]
set: real Wz_1 = 0.0; #Z component of the absolute angular velocity [rad/s]
#node: 2
set: real Px_2 = 0.018683478687078307; #X component of the absolute position [m]
set: real Py_2 = -0.05533171845235879; #Y component of the absolute position [m]
set: real Pz_2 = 0.1768528076947657; #Z component of the absolute position [m]
set: real Vx_2 = 0.0; #X component of the absolute velocity [m/s]
set: real Vy_2 = 0.0; #Y component of the absolute velocity [m/s]
set: real Vz_2 = 0.0; #Z component of the absolute velocity [m/s]
set: real Wx_2 = 0.0; #X component of the absolute angular velocity [rad/s]
set: real Wy_2 = 0.0; #Y component of the absolute angular velocity [rad/s]
set: real Wz_2 = 0.0; #Z component of the absolute angular velocity [rad/s]
#node: 3
set: real Px_3 = 0.2890983348369078; #X component of the absolute position [m]
set: real Py_3 = -0.06156645049450425; #Y component of the absolute position [m]
set: real Pz_3 = 0.09724597715885096; #Z component of the absolute position [m]
set: real Vx_3 = 0.0; #X component of the absolute velocity [m/s]
set: real Vy_3 = 0.0; #Y component of the absolute velocity [m/s]
set: real Vz_3 = 0.0; #Z component of the absolute velocity [m/s]
set: real Wx_3 = 0.0; #X component of the absolute angular velocity [rad/s]
set: real Wy_3 = 0.0; #Y component of the absolute angular velocity [rad/s]
set: real Wz_3 = 0.0; #Z component of the absolute angular velocity [rad/s]
#node: 4
set: real Px_4 = 0.11637356459110539; #X component of the absolute position [m]
set: real Py_4 = -0.019655254070140387; #Y component of the absolute position [m]
set: real Pz_4 = 0.20651079866339145; #Z component of the absolute position [m]
set: real Vx_4 = 0.0; #X component of the absolute velocity [m/s]
set: real Vy_4 = 0.0; #Y component of the absolute velocity [m/s]
set: real Vz_4 = 0.0; #Z component of the absolute velocity [m/s]
set: real Wx_4 = 0.0; #X component of the absolute angular velocity [rad/s]
set: real Wy_4 = 0.0; #Y component of the absolute angular velocity [rad/s]
set: real Wz_4 = 0.0; #Z component of the absolute angular velocity [rad/s]
#node: 5
set: real Px_5 = 0.15064540729834192; #X component of the absolute position [m]
set: real Py_5 = -0.020536937096322302; #Y component of the absolute position [m]
set: real Pz_5 = 0.06548008210568429; #Z component of the absolute position [m]
set: real Vx_5 = 0.0; #X component of the absolute velocity [m/s]
set: real Vy_5 = 0.0; #Y component of the absolute velocity [m/s]
set: real Vz_5 = 0.0; #Z component of the absolute velocity [m/s]
set: real Wx_5 = 0.0; #X component of the absolute angular velocity [rad/s]
set: real Wy_5 = 0.0; #Y component of the absolute angular velocity [rad/s]
set: real Wz_5 = 0.0; #Z component of the absolute angular velocity [rad/s]
#-----------------------------------------------------------------------------
# [Intermediate Variables]
#Moments of inertia and relative center of mass
#body 2:
set: real Ixx_2 = 6.927961737800001e-05; #moment of inertia [kg*m^2]
set: real Iyy_2 = 5.6689424982e-05; #moment of inertia [kg*m^2]
set: real Izz_2 = 2.9053392577e-05; #moment of inertia [kg*m^2]
set: real Rx_2 = 0.0; #X component of the relative center of mass [m]
set: real Ry_2 = 0.0; #Y component of the relative center of mass [m]
set: real Rz_2 = 0.0; #Z component of the relative center of mass [m]
#body 4:
set: real Ixx_4 = 7.9157004521e-05; #moment of inertia [kg*m^2]
set: real Iyy_4 = 7.769349168e-05; #moment of inertia [kg*m^2]
set: real Izz_4 = 3.339121993e-06; #moment of inertia [kg*m^2]
set: real Rx_4 = 0.0; #X component of the relative center of mass [m]
set: real Ry_4 = 0.0; #Y component of the relative center of mass [m]
set: real Rz_4 = 0.0; #Z component of the relative center of mass [m]
#body 5:
set: real Ixx_5 = 7.9157004521e-05; #moment of inertia [kg*m^2]
set: real Iyy_5 = 7.769349168e-05; #moment of inertia [kg*m^2]
set: real Izz_5 = 3.339121993e-06; #moment of inertia [kg*m^2]
set: real Rx_5 = 0.0; #X component of the relative center of mass [m]
set: real Ry_5 = 0.0; #Y component of the relative center of mass [m]
set: real Rz_5 = 0.0; #Z component of the relative center of mass [m]
#-----------------------------------------------------------------------------
# [Nodes Block]
begin: nodes;
structural: structural_node_1,
static,
Px_1, Py_1, Pz_1, #<absolute_position> [m]
3, -0.3539135011019427, 0.9158836712023025, 0.18947911379030236, 2, -0.5084786583487672, -0.018385530501657588, -0.8608782877224926, #<absolute_orientation_matrix>
Vx_1, Vy_1, Vz_1, #<absolute_velocity> [m/s]
Wx_1, Wy_1, Wz_1; #<absolute_angular_velocity> [rad/s]
structural: structural_node_2,
dynamic,
Px_2, Py_2, Pz_2, #<absolute_position> [m]
3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0, #<absolute_orientation_matrix>
Vx_2, Vy_2, Vz_2, #<absolute_velocity> [m/s]
Wx_2, Wy_2, Wz_2; #<absolute_angular_velocity> [rad/s]
structural: structural_node_3,
static,
Px_3, Py_3, Pz_3, #<absolute_position> [m]
3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0, #<absolute_orientation_matrix>
Vx_3, Vy_3, Vz_3, #<absolute_velocity> [m/s]
Wx_3, Wy_3, Wz_3; #<absolute_angular_velocity> [rad/s]
structural: structural_node_4,
dynamic,
Px_4, Py_4, Pz_4, #<absolute_position> [m]
3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0, #<absolute_orientation_matrix>
Vx_4, Vy_4, Vz_4, #<absolute_velocity> [m/s]
Wx_4, Wy_4, Wz_4; #<absolute_angular_velocity> [rad/s]
structural: structural_node_5,
dynamic,
Px_5, Py_5, Pz_5, #<absolute_position> [m]
3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0, #<absolute_orientation_matrix>
Vx_5, Vy_5, Vz_5, #<absolute_velocity> [m/s]
Wx_5, Wy_5, Wz_5; #<absolute_angular_velocity> [rad/s]
end: nodes;
#-----------------------------------------------------------------------------
# [Elements Block]
begin: elements;
#-----------------------------------------------------------------------------
# [Bodies]
body: body_2,
structural_node_2, #<node_label>
mass_2, #<mass> [kg]
Rx_2, Ry_2, Rz_2, #<relative_center_of_mass> [m]
diag, Ixx_2, Iyy_2, Izz_2, #<inertia matrix> [kg*m^2]
orientation, 3, -0.35, 0.91, 0.21, 2, 0.78, 0.4, -0.47;
body: body_4,
structural_node_4, #<node_label>
mass_4, #<mass> [kg]
Rx_4, Ry_4, Rz_4, #<relative_center_of_mass> [m]
diag, Ixx_4, Iyy_4, Izz_4, #<inertia matrix> [kg*m^2]
orientation, 3, 0.78, 0.4, -0.47, 2, -0.36, 0.91, 0.19;
body: body_5,
structural_node_5, #<node_label>
mass_5, #<mass> [kg]
Rx_5, Ry_5, Rz_5, #<relative_center_of_mass> [m]
diag, Ixx_5, Iyy_5, Izz_5, #<inertia matrix> [kg*m^2]
orientation, 3, -0.36, 0.91, 0.19, 2, 0.78, 0.4, -0.47;
#-----------------------------------------------------------------------------
# [Joints]
joint: joint_1,
clamp,
structural_node_1, #<node_label>
0.16912189837562464, -0.10055206743263254, 0.07867737409397452, #<absolute_pin_position> [m]
3, -0.3539135011019427, 0.9158836712023025, 0.18947911379030236, 2, -0.5084786583487672, -0.018385530501657588, -0.8608782877224926; #<absolute_orientation_matrix>
joint: joint_2,
axial rotation,
structural_node_1, #<node_1_label>
1.0407603667772492e-11, -0.05247682460581396, -0.00025357557055826873, #<relative_offset_1> [m]
orientation, 3, 1.1102230246251565e-16, -1.0, 0.0, 2, guess, #<relative_orientation_matrix_1>
structural_node_2, #<node_2_label>
0.006998226646402806, -0.00490348349806041, 0.007426083408032554, #<relative_offset_2> [m]
orientation, 3, 0.5084786344413901, 0.01838554762064229, 0.8608783014778036, 2, guess, #<relative_orientation_matrix_2>
string, "model::drive(1, Time)"; #<angular_velocity> [rad/s]
joint: joint_3,
clamp,
structural_node_3, #<node_label>
0.2890983348369078, -0.06156645049450425, 0.09724597715885096, #<absolute_pin_position> [m]
3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0; #<absolute_orientation_matrix>
joint: joint_4,
revolute hinge,
structural_node_2, #<node_1_label>
-0.0011629534118987692, 0.02262071327533141, 0.01746668757489371, #<relative_position_1> [m]
orientation, 3, 0.5084786344412178, 0.018385547620640152, 0.8608783014779054, 2, guess, #<relative_pin_orientation_matrix_1>
structural_node_4, #<node_2_label>
-0.031347177833029705, -0.01617494903756937, 0.018860685712244078, #<relative_position_2> [m]
orientation, 3, 0.5084786455601428, 0.018385495401303797, 0.860878296025734, 2, guess; #<relative_pin_orientation_matrix_2>
joint: joint_5,
revolute hinge,
structural_node_4, #<node_1_label>
0.03388957106083931, 0.016266876514581658, -0.01455629423212079, #<relative_position_1> [m]
orientation, 3, 0.50847864556046, 0.0183854954014063, 0.8608782960255446, 2, guess, #<relative_pin_orientation_matrix_1>
structural_node_5, #<node_2_label>
-0.016813818553224735, 0.036484433510506876, 0.003343892503690739, #<relative_position_2> [m]
orientation, 3, 0.5084787180221569, 0.01838550036990011, 0.8608782531198544, 2, guess; #<relative_pin_orientation_matrix_2>
joint: joint_7,
revolute hinge,
structural_node_3, #<node_1_label>
1.1368683772161603e-16, 0.0, -1.4210854715202004e-17, #<relative_position_1> [m]
orientation, 3, 0.5094306516594838, 0.018659363391322903, 0.8603093858070039, 2, guess, #<relative_pin_orientation_matrix_1>
structural_node_5, #<node_2_label>
0.014271424963118534, -0.03657636101236503, -0.007648283769292526, #<relative_position_2> [m]
orientation, 3, 0.5084787180221835, 0.018385500369866165, 0.8608782531198396, 2, guess; #<relative_pin_orientation_matrix_2>
#-----------------------------------------------------------------------------
# [Drive callers]
drive caller: 1, name,"drive:1", ramp, 5.0, 0.25, 4.0, 0.0;
end: elements;

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#-----------------------------------------------------------------------------
# [Data Block]
begin: data;
problem: initial value;
end: data;
#-----------------------------------------------------------------------------
# [Problem Block]
begin: initial value;
initial time: 0.0;
final time: 8.0;
time step: 0.01;
max iterations: 100;
tolerance: 1e-06;
derivatives tolerance: 0.0001;
derivatives max iterations: 100;
derivatives coefficient: auto;
end: initial value;
#-----------------------------------------------------------------------------
# [Control Data Block]
begin: control data;
max iterations: 1000;
default orientation: orientation matrix;
omega rotates: no;
print: none;
initial stiffness: 1.0, 1.0;
structural nodes: 5;
rigid bodies: 3;
joints: 6;
end: control data;
#-----------------------------------------------------------------------------
# [Design Variables]
#Generic bodies
#body: 2
set: integer body_2 = 2; #body label
set: real mass_2 = 0.24147734685710437; #mass [kg]
set: real volume_2 = 3.056675276672207e-05; #volume [m^3]
#body: 4
set: integer body_4 = 4; #body label
set: real mass_4 = 0.11253654770310718; #mass [kg]
set: real volume_4 = 1.4245132620646478e-05; #volume [m^3]
#body: 5
set: integer body_5 = 5; #body label
set: real mass_5 = 0.11253654770310723; #mass [kg]
set: real volume_5 = 1.4245132620646483e-05; #volume [m^3]
#Nodes
#node: 1
set: integer structural_node_1 = 1; #node label
#node: 2
set: integer structural_node_2 = 2; #node label
#node: 3
set: integer structural_node_3 = 3; #node label
#node: 4
set: integer structural_node_4 = 4; #node label
#node: 5
set: integer structural_node_5 = 5; #node label
#Joints
#joint: 1
set: integer joint_1 = 1; #joint label
#joint: 2
set: integer joint_2 = 2; #joint label
#joint: 3
set: integer joint_3 = 3; #joint label
#joint: 4
set: integer joint_4 = 4; #joint label
#joint: 5
set: integer joint_5 = 5; #joint label
#joint: 6
set: integer joint_6 = 6; #joint label
#Nodes: initial conditions
#node: 1
set: real Px_1 = 0.16912189837562464; #X component of the absolute position [m]
set: real Py_1 = -0.10055206743263254; #Y component of the absolute position [m]
set: real Pz_1 = 0.07867737409397452; #Z component of the absolute position [m]
set: real Vx_1 = 0.0; #X component of the absolute velocity [m/s]
set: real Vy_1 = 0.0; #Y component of the absolute velocity [m/s]
set: real Vz_1 = 0.0; #Z component of the absolute velocity [m/s]
set: real Wx_1 = 0.0; #X component of the absolute angular velocity [rad/s]
set: real Wy_1 = 0.0; #Y component of the absolute angular velocity [rad/s]
set: real Wz_1 = 0.0; #Z component of the absolute angular velocity [rad/s]
#node: 2
set: real Px_2 = 0.018683478687078307; #X component of the absolute position [m]
set: real Py_2 = -0.05533171845235879; #Y component of the absolute position [m]
set: real Pz_2 = 0.1768528076947657; #Z component of the absolute position [m]
set: real Vx_2 = 0.0; #X component of the absolute velocity [m/s]
set: real Vy_2 = 0.0; #Y component of the absolute velocity [m/s]
set: real Vz_2 = 0.0; #Z component of the absolute velocity [m/s]
set: real Wx_2 = 0.0; #X component of the absolute angular velocity [rad/s]
set: real Wy_2 = 0.0; #Y component of the absolute angular velocity [rad/s]
set: real Wz_2 = 0.0; #Z component of the absolute angular velocity [rad/s]
#node: 3
set: real Px_3 = 0.2890983348369078; #X component of the absolute position [m]
set: real Py_3 = -0.06156645049450425; #Y component of the absolute position [m]
set: real Pz_3 = 0.09724597715885096; #Z component of the absolute position [m]
set: real Vx_3 = 0.0; #X component of the absolute velocity [m/s]
set: real Vy_3 = 0.0; #Y component of the absolute velocity [m/s]
set: real Vz_3 = 0.0; #Z component of the absolute velocity [m/s]
set: real Wx_3 = 0.0; #X component of the absolute angular velocity [rad/s]
set: real Wy_3 = 0.0; #Y component of the absolute angular velocity [rad/s]
set: real Wz_3 = 0.0; #Z component of the absolute angular velocity [rad/s]
#node: 4
set: real Px_4 = 0.11637356459110539; #X component of the absolute position [m]
set: real Py_4 = -0.019655254070140387; #Y component of the absolute position [m]
set: real Pz_4 = 0.20651079866339145; #Z component of the absolute position [m]
set: real Vx_4 = 0.0; #X component of the absolute velocity [m/s]
set: real Vy_4 = 0.0; #Y component of the absolute velocity [m/s]
set: real Vz_4 = 0.0; #Z component of the absolute velocity [m/s]
set: real Wx_4 = 0.0; #X component of the absolute angular velocity [rad/s]
set: real Wy_4 = 0.0; #Y component of the absolute angular velocity [rad/s]
set: real Wz_4 = 0.0; #Z component of the absolute angular velocity [rad/s]
#node: 5
set: real Px_5 = 0.15064540729834192; #X component of the absolute position [m]
set: real Py_5 = -0.020536937096322302; #Y component of the absolute position [m]
set: real Pz_5 = 0.06548008210568429; #Z component of the absolute position [m]
set: real Vx_5 = 0.0; #X component of the absolute velocity [m/s]
set: real Vy_5 = 0.0; #Y component of the absolute velocity [m/s]
set: real Vz_5 = 0.0; #Z component of the absolute velocity [m/s]
set: real Wx_5 = 0.0; #X component of the absolute angular velocity [rad/s]
set: real Wy_5 = 0.0; #Y component of the absolute angular velocity [rad/s]
set: real Wz_5 = 0.0; #Z component of the absolute angular velocity [rad/s]
#-----------------------------------------------------------------------------
# [Intermediate Variables]
#Moments of inertia and relative center of mass
#body 2:
set: real Ixx_2 = 6.927961737800001e-05; #moment of inertia [kg*m^2]
set: real Iyy_2 = 5.6689424982e-05; #moment of inertia [kg*m^2]
set: real Izz_2 = 2.9053392577e-05; #moment of inertia [kg*m^2]
set: real Rx_2 = 0.0; #X component of the relative center of mass [m]
set: real Ry_2 = 0.0; #Y component of the relative center of mass [m]
set: real Rz_2 = 0.0; #Z component of the relative center of mass [m]
#body 4:
set: real Ixx_4 = 7.9157004521e-05; #moment of inertia [kg*m^2]
set: real Iyy_4 = 7.769349168e-05; #moment of inertia [kg*m^2]
set: real Izz_4 = 3.339121993e-06; #moment of inertia [kg*m^2]
set: real Rx_4 = 0.0; #X component of the relative center of mass [m]
set: real Ry_4 = 0.0; #Y component of the relative center of mass [m]
set: real Rz_4 = 0.0; #Z component of the relative center of mass [m]
#body 5:
set: real Ixx_5 = 7.9157004521e-05; #moment of inertia [kg*m^2]
set: real Iyy_5 = 7.769349168e-05; #moment of inertia [kg*m^2]
set: real Izz_5 = 3.339121993e-06; #moment of inertia [kg*m^2]
set: real Rx_5 = 0.0; #X component of the relative center of mass [m]
set: real Ry_5 = 0.0; #Y component of the relative center of mass [m]
set: real Rz_5 = 0.0; #Z component of the relative center of mass [m]
#-----------------------------------------------------------------------------
# [Nodes Block]
begin: nodes;
structural: structural_node_1,
static,
Px_1, Py_1, Pz_1, #<absolute_position> [m]
3, -0.3539135011019427, 0.9158836712023025, 0.18947911379030236, 2, -0.5084786583487672, -0.018385530501657588, -0.8608782877224926, #<absolute_orientation_matrix>
Vx_1, Vy_1, Vz_1, #<absolute_velocity> [m/s]
Wx_1, Wy_1, Wz_1; #<absolute_angular_velocity> [rad/s]
structural: structural_node_2,
dynamic,
Px_2, Py_2, Pz_2, #<absolute_position> [m]
3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0, #<absolute_orientation_matrix>
Vx_2, Vy_2, Vz_2, #<absolute_velocity> [m/s]
Wx_2, Wy_2, Wz_2; #<absolute_angular_velocity> [rad/s]
structural: structural_node_3,
static,
Px_3, Py_3, Pz_3, #<absolute_position> [m]
3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0, #<absolute_orientation_matrix>
Vx_3, Vy_3, Vz_3, #<absolute_velocity> [m/s]
Wx_3, Wy_3, Wz_3; #<absolute_angular_velocity> [rad/s]
structural: structural_node_4,
dynamic,
Px_4, Py_4, Pz_4, #<absolute_position> [m]
3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0, #<absolute_orientation_matrix>
Vx_4, Vy_4, Vz_4, #<absolute_velocity> [m/s]
Wx_4, Wy_4, Wz_4; #<absolute_angular_velocity> [rad/s]
structural: structural_node_5,
dynamic,
Px_5, Py_5, Pz_5, #<absolute_position> [m]
3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0, #<absolute_orientation_matrix>
Vx_5, Vy_5, Vz_5, #<absolute_velocity> [m/s]
Wx_5, Wy_5, Wz_5; #<absolute_angular_velocity> [rad/s]
end: nodes;
#-----------------------------------------------------------------------------
# [Elements Block]
begin: elements;
#-----------------------------------------------------------------------------
# [Bodies]
body: body_2,
structural_node_2, #<node_label>
mass_2, #<mass> [kg]
Rx_2, Ry_2, Rz_2, #<relative_center_of_mass> [m]
diag, Ixx_2, Iyy_2, Izz_2, #<inertia matrix> [kg*m^2]
orientation, 3, -0.35, 0.91, 0.21, 2, 0.78, 0.4, -0.47;
body: body_4,
structural_node_4, #<node_label>
mass_4, #<mass> [kg]
Rx_4, Ry_4, Rz_4, #<relative_center_of_mass> [m]
diag, Ixx_4, Iyy_4, Izz_4, #<inertia matrix> [kg*m^2]
orientation, 3, 0.78, 0.4, -0.47, 2, -0.36, 0.91, 0.19;
body: body_5,
structural_node_5, #<node_label>
mass_5, #<mass> [kg]
Rx_5, Ry_5, Rz_5, #<relative_center_of_mass> [m]
diag, Ixx_5, Iyy_5, Izz_5, #<inertia matrix> [kg*m^2]
orientation, 3, -0.36, 0.91, 0.19, 2, 0.78, 0.4, -0.47;
#-----------------------------------------------------------------------------
# [Joints]
joint: joint_1,
clamp,
structural_node_1, #<node_label>
0.16912189837562464, -0.10055206743263254, 0.07867737409397452, #<absolute_pin_position> [m]
3, -0.3539135011019427, 0.9158836712023025, 0.18947911379030236, 2, -0.5084786583487672, -0.018385530501657588, -0.8608782877224926; #<absolute_orientation_matrix>
joint: joint_2,
axial rotation,
structural_node_1, #<node_1_label>
1.0407603667772492e-11, -0.05247682460581396, -0.00025357557055826873, #<relative_offset_1> [m]
orientation, 3, 1.1102230246251565e-16, -1.0, 0.0, 2, guess, #<relative_orientation_matrix_1>
structural_node_2, #<node_2_label>
0.006998226646402806, -0.00490348349806041, 0.007426083408032554, #<relative_offset_2> [m]
orientation, 3, 0.5084786344413901, 0.01838554762064229, 0.8608783014778036, 2, guess, #<relative_orientation_matrix_2>
string, "model::drive(1, Time)"; #<angular_velocity> [rad/s]
joint: joint_3,
clamp,
structural_node_3, #<node_label>
0.2890983348369078, -0.06156645049450425, 0.09724597715885096, #<absolute_pin_position> [m]
3, 0.0, 0.0, 1.0, 2, 0.0, 1.0, 0.0; #<absolute_orientation_matrix>
joint: joint_4,
revolute hinge,
structural_node_2, #<node_1_label>
-0.0011629534118987692, 0.02262071327533141, 0.01746668757489371, #<relative_position_1> [m]
orientation, 3, 0.5084786344412178, 0.018385547620640152, 0.8608783014779054, 2, guess, #<relative_pin_orientation_matrix_1>
structural_node_4, #<node_2_label>
-0.031347177833029705, -0.01617494903756937, 0.018860685712244078, #<relative_position_2> [m]
orientation, 3, 0.5084786455601428, 0.018385495401303797, 0.860878296025734, 2, guess; #<relative_pin_orientation_matrix_2>
joint: joint_5,
revolute hinge,
structural_node_4, #<node_1_label>
0.03388957106083931, 0.016266876514581658, -0.01455629423212079, #<relative_position_1> [m]
orientation, 3, 0.50847864556046, 0.0183854954014063, 0.8608782960255446, 2, guess, #<relative_pin_orientation_matrix_1>
structural_node_5, #<node_2_label>
-0.016813818553224735, 0.036484433510506876, 0.003343892503690739, #<relative_position_2> [m]
orientation, 3, 0.5084787180221569, 0.01838550036990011, 0.8608782531198544, 2, guess; #<relative_pin_orientation_matrix_2>
joint: joint_6,
in line,
structural_node_3, #<node_1_label>
0.0, 0.0, 0.0, #<relative_line_position> [m]
3, 0.5094306516594838, 0.018659363391322903, 0.8603093858070039, 2, guess, #<relative_orientation>
structural_node_5, #<node_2_label>
offset, 0.014271424963118534, -0.03657636101236503, -0.007648283769292526; #<relative_offset> [m]
#-----------------------------------------------------------------------------
# [Drive callers]
drive caller: 1, name,"drive:1", ramp, 5.0, 0.25, 4.0, 0.0;
end: elements;

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@@ -26,26 +26,25 @@ void sharedptrTest();
int main()
{
ASMTAssembly::readWriteFile("failingsolve.asmt");
ASMTAssembly::runFile("cirpendu2.asmt"); //Under constrained. Testing ICKine.
ASMTAssembly::runFile("quasikine.asmt"); //Under constrained. Testing ICKine.
ASMTAssembly::readWriteFile("piston.asmt");
//MBDynSystem::runFile("MBDynCaseDebug2.mbd");
ASMTAssembly::runFile("../testapp/cirpendu2.asmt"); //Under constrained. Testing ICKine.
ASMTAssembly::runFile("../testapp/quasikine.asmt"); //Under constrained. Testing ICKine.
ASMTAssembly::readWriteFile("../testapp/piston.asmt");
//MBDynSystem::runFile("../testapp/MBDynCaseDebug2.mbd");
//return 0;
MBDynSystem::runFile("MBDynCase2.mbd");
MBDynSystem::runFile("MBDynCase.mbd");
MBDynSystem::runFile("CrankSlider2.mbd");
//MBDynSystem::runFile("crank_slider.mbd"); //Needs integration of product
MBDynSystem::runFile("../testapp/MBDynCase2.mbd");
//MBDynSystem::runFile("../testapp/MBDynCase.mbd"); //Very large but works
MBDynSystem::runFile("../testapp/CrankSlider2.mbd");
//MBDynSystem::runFile("../testapp/crank_slider.mbd"); //Needs integration of product
////ASMTAssembly::runSinglePendulumSuperSimplified(); //Mass is missing
////ASMTAssembly::runSinglePendulumSuperSimplified2(); //DOF has infinite acceleration due to zero mass and inertias
ASMTAssembly::runSinglePendulumSimplified();
ASMTAssembly::runSinglePendulum();
ASMTAssembly::runFile("../testapp/piston.asmt");
ASMTAssembly::runFile("../testapp/00backhoe.asmt");
//ASMTAssembly::runFile("circular.asmt"); //Needs checking
//ASMTAssembly::runFile("engine1.asmt"); //Needs checking
//ASMTAssembly::runFile("../testapp/circular.asmt"); //Needs checking
//ASMTAssembly::runFile("../testapp/engine1.asmt"); //Needs checking
ASMTAssembly::runFile("../testapp/fourbar.asmt");
//ASMTAssembly::runFile("fourbot.asmt"); //Very large but works
//ASMTAssembly::runFile("../testapp/fourbot.asmt"); //Very large but works
ASMTAssembly::runFile("../testapp/wobpump.asmt");
auto cadSystem = std::make_shared<CADSystem>();

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# crank_slider.mbd
#-----------------------------------------------------------------------------
# [Data Block]
begin: data;
problem: initial value;
end: data;
#-----------------------------------------------------------------------------
# [<Problem> Block]
begin: initial value;
initial time: 0.;
final time: 5.;
time step: 1.e-1;
max iterations: 10;
tolerance: 1.e-6;
end: initial value;
#-----------------------------------------------------------------------------
# [Control Data Block]
begin: control data;
structural nodes: 4;
rigid bodies: 3;
joints: 6;
end: control data;
#-----------------------------------------------------------------------------
# Design Variables
set: real Mass_Crank = 1.;
set: real Mass_Conrod = 1.;
set: real Mass_Slider = 1.;
set: real Length_Crank = 0.2;
set: real Length_Conrod = 0.4;
set: real Offset_Slider = 0.05;
#-----------------------------------------------------------------------------
# Reference Labels
set: integer Ref_Conrod = 1;
# Node Labels
set: integer Node_Ground = 1;
set: integer Node_Crank = 2;
set: integer Node_Conrod = 3;
set: integer Node_Slider = 4;
# Body Labels
set: integer Body_Crank = 1;
set: integer Body_Conrod = 2;
set: integer Body_Slider = 3;
# Joint Labels
set: integer JoClamp_Ground = 1;
set: integer JoAxrot_Ground_Crank = 2;
set: integer JoRevh_Crank_Conrod = 3;
set: integer JoInlin_Conrod_Slider = 4;
set: integer JoInlin_Ground_Slider = 5;
set: integer JoPrism_Ground_Slider = 6;
#-----------------------------------------------------------------------------
# Intermediate Variables
set: real Izz_Crank = Mass_Crank*Length_Crank^2./12.;
set: real Izz_Conrod = Mass_Conrod*Length_Conrod^2./12.;
#-----------------------------------------------------------------------------
# References
reference: Ref_Conrod,
Length_Crank, 0., 0., # absolute position
euler, 0., 0., asin(Offset_Slider/Length_Conrod), # absolute orientation
null, # absolute velocity
null; # absolute angular velocity
#-----------------------------------------------------------------------------
# [Nodes Block]
begin: nodes;
#-----------------------------------------------------------------------------
# Nodes
structural: Node_Ground, static,
0., 0., 0., # absolute position
eye, # absolute orientation
null, # absolute velocity
null; # absolute angular velocity
structural: Node_Crank, dynamic,
Length_Crank/2., 0., 0., # absolute position
eye, # absolute orientation
null, # absolute velocity
null; # absolute angular velocity
structural: Node_Conrod, dynamic,
reference, Ref_Conrod, Length_Conrod/2., 0., 0., # absolute position
reference, Ref_Conrod, eye, # absolute orientation
null, # absolute velocity
null; # absolute angular velocity
structural: Node_Slider, dynamic,
reference, Ref_Conrod, Length_Conrod, 0., 0., # absolute position
eye, # absolute orientation
null, # absolute velocity
null; # absolute angular velocity
end: nodes;
#-----------------------------------------------------------------------------
# [Elements Block]
begin: elements;
#-----------------------------------------------------------------------------
# Bodies
body: Body_Crank, Node_Crank,
Mass_Crank, # mass
null, # relative center of mass
diag, 1., 1., Izz_Crank; # inertia matrix
body: Body_Conrod, Node_Conrod,
Mass_Conrod, # mass
null, # relative center of mass
diag, 1., 1., Izz_Conrod; # inertia matrix
body: Body_Slider, Node_Slider,
Mass_Slider, # mass
null, # relative center of mass
eye; # inertia matrix
#-----------------------------------------------------------------------------
# Joints
joint: JoClamp_Ground,
clamp,
Node_Ground,
null, # absolute position
eye; # absolute orientation
joint: JoAxrot_Ground_Crank,
axial rotation,
Node_Ground,
null, # relative offset
hinge, eye, # relative orientation
Node_Crank,
-Length_Crank/2., 0., 0., # relative offset
hinge, eye, # relative orientation
ramp, 2.*pi, 0., 1., 0.; # angular velocity
joint: JoRevh_Crank_Conrod,
revolute hinge,
Node_Crank,
reference, Ref_Conrod, null, # relative offset
hinge, reference, Ref_Conrod, eye, # relative axis orientation
Node_Conrod,
reference, Ref_Conrod, null, # relative offset
hinge, reference, Ref_Conrod, eye; # relative axis orientation
joint: JoInlin_Conrod_Slider,
in line,
Node_Conrod,
Length_Conrod/2., 0., 0., # relative line position
eye, # relative orientation
Node_Slider;
joint: JoInlin_Ground_Slider,
in line,
Node_Ground,
0., Offset_Slider, 0., # relative line position
1, 0., 0., -1., 3, 1., 0., 0., # relative orientation
Node_Slider;
joint: JoPrism_Ground_Slider,
prismatic,
Node_Ground,
Node_Slider;
end: elements;

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# crank_slider.mbd
#-----------------------------------------------------------------------------
# [Data Block]
begin: data;
problem: initial value;
end: data;
#-----------------------------------------------------------------------------
# [<Problem> Block]
begin: initial value;
initial time: 0.;
final time: 1.;
time step: 1.e-1;
max iterations: 10;
tolerance: 1.e-6;
end: initial value;
#-----------------------------------------------------------------------------
# [Control Data Block]
begin: control data;
structural nodes: 4;
rigid bodies: 3;
joints: 6;
end: control data;
#-----------------------------------------------------------------------------
# Design Variables
set: real Mass_Crank = 1.;
set: real Mass_Conrod = 1.;
set: real Mass_Slider = 1.;
set: real Length_Crank = 0.2;
set: real Length_Conrod = 0.4;
set: real Offset_Slider = 0.05;
#-----------------------------------------------------------------------------
# Reference Labels
set: integer Ref_Conrod = 1;
# Node Labels
set: integer Node_Ground = 1;
set: integer Node_Crank = 2;
set: integer Node_Conrod = 3;
set: integer Node_Slider = 4;
# Body Labels
set: integer Body_Crank = 1;
set: integer Body_Conrod = 2;
set: integer Body_Slider = 3;
# Joint Labels
set: integer JoClamp_Ground = 1;
set: integer JoAxrot_Ground_Crank = 2;
set: integer JoRevh_Crank_Conrod = 3;
set: integer JoInlin_Conrod_Slider = 4;
set: integer JoInlin_Ground_Slider = 5;
set: integer JoPrism_Ground_Slider = 6;
#-----------------------------------------------------------------------------
# Intermediate Variables
set: real Izz_Crank = Mass_Crank*Length_Crank^2./12.;
set: real Izz_Conrod = Mass_Conrod*Length_Conrod^2./12.;
#-----------------------------------------------------------------------------
# References
reference: Ref_Conrod,
Length_Crank, 0., 0., # absolute position
euler, 0., 0., asin(Offset_Slider/Length_Conrod), # absolute orientation
null, # absolute velocity
null; # absolute angular velocity
#-----------------------------------------------------------------------------
# [Nodes Block]
begin: nodes;
#-----------------------------------------------------------------------------
# Nodes
structural: Node_Ground, static,
0., 0., 0., # absolute position
eye, # absolute orientation
null, # absolute velocity
null; # absolute angular velocity
structural: Node_Crank, dynamic,
Length_Crank/2., 0., 0., # absolute position
eye, # absolute orientation
null, # absolute velocity
null; # absolute angular velocity
structural: Node_Conrod, dynamic,
reference, Ref_Conrod, Length_Conrod/2., 0., 0., # absolute position
reference, Ref_Conrod, eye, # absolute orientation
null, # absolute velocity
null; # absolute angular velocity
structural: Node_Slider, dynamic,
reference, Ref_Conrod, Length_Conrod, 0., 0., # absolute position
eye, # absolute orientation
null, # absolute velocity
null; # absolute angular velocity
end: nodes;
#-----------------------------------------------------------------------------
# [Elements Block]
begin: elements;
#-----------------------------------------------------------------------------
# Bodies
body: Body_Crank, Node_Crank,
Mass_Crank, # mass
null, # relative center of mass
diag, 1., 1., Izz_Crank; # inertia matrix
body: Body_Conrod, Node_Conrod,
Mass_Conrod, # mass
null, # relative center of mass
diag, 1., 1., Izz_Conrod; # inertia matrix
body: Body_Slider, Node_Slider,
Mass_Slider, # mass
null, # relative center of mass
eye; # inertia matrix
#-----------------------------------------------------------------------------
# Joints
joint: JoClamp_Ground,
clamp,
Node_Ground,
null, # absolute position
eye; # absolute orientation
joint: JoAxrot_Ground_Crank,
axial rotation,
Node_Ground,
null, # relative offset
hinge, eye, # relative orientation
Node_Crank,
-Length_Crank/2., 0., 0., # relative offset
hinge, eye, # relative orientation
ramp, 2.*pi, 0., 1., 0.; # angular velocity
joint: JoRevh_Crank_Conrod,
revolute hinge,
Node_Crank,
reference, Ref_Conrod, null, # relative offset
hinge, reference, Ref_Conrod, eye, # relative axis orientation
Node_Conrod,
reference, Ref_Conrod, null, # relative offset
hinge, reference, Ref_Conrod, eye; # relative axis orientation
joint: JoInlin_Conrod_Slider,
in line,
Node_Conrod,
Length_Conrod/2., 0., 0., # relative line position
eye, # relative orientation
Node_Slider;
joint: JoInlin_Ground_Slider,
in line,
Node_Ground,
0., Offset_Slider, 0., # relative line position
1, 0., 0., -1., 3, 1., 0., 0., # relative orientation
Node_Slider;
joint: JoPrism_Ground_Slider,
prismatic,
Node_Ground,
Node_Slider;
end: elements;

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