How correctly use Simple Variable Mass 3DOF (Body Axes) block?
Hello,
As in the title, I need to simulate an aircraft mission with varying mass. In the Aerospace Blockset, I’ve so found the Simple Variable Mass (3DOF). I have some problems in interpreting these inertia definitions:
Empty inertia — Body inertia when fuel tank is full
0.5 (default) | scalar
Body inertia when the fuel tank is full, specified as a double scalar.
and
Full inertia — Full inertia
3.0 (default) | scalar
Full inertia of the body, specified as a scalar.
My concerns involves the difference between Empty and full inertia. From the documentation, they seem to be the same. Can anyone help me?
Thanks.Hello,
As in the title, I need to simulate an aircraft mission with varying mass. In the Aerospace Blockset, I’ve so found the Simple Variable Mass (3DOF). I have some problems in interpreting these inertia definitions:
Empty inertia — Body inertia when fuel tank is full
0.5 (default) | scalar
Body inertia when the fuel tank is full, specified as a double scalar.
and
Full inertia — Full inertia
3.0 (default) | scalar
Full inertia of the body, specified as a scalar.
My concerns involves the difference between Empty and full inertia. From the documentation, they seem to be the same. Can anyone help me?
Thanks. Hello,
As in the title, I need to simulate an aircraft mission with varying mass. In the Aerospace Blockset, I’ve so found the Simple Variable Mass (3DOF). I have some problems in interpreting these inertia definitions:
Empty inertia — Body inertia when fuel tank is full
0.5 (default) | scalar
Body inertia when the fuel tank is full, specified as a double scalar.
and
Full inertia — Full inertia
3.0 (default) | scalar
Full inertia of the body, specified as a scalar.
My concerns involves the difference between Empty and full inertia. From the documentation, they seem to be the same. Can anyone help me?
Thanks. 3dof, varying mass, aerospace, simulink, simulation MATLAB Answers — New Questions