Estimate Inertia Tensor
Calculation of the inertia tensor.
Description
The Estimate Inertia Tensor block calculates the inertia tensor as a function of mass and the rate of change of the inertia tensor as a linear function of the rate of change of mass. Linear interpolation is used to determine the inertia tensor.
Ports
Parameters
Full mass - full mass
2.0 (by default) | scalar
The total mass of the aircraft.
Empty mass - mass without fuel
1.0 (By default) | scalar
The mass of the aircraft without fuel.
Full inertia matrix - inertia tensor at full mass
[1.0 0.0 0.0 0.0; 0.0 1.0 0.0; 0.0 0.0 1.0] (by default) | ` 3 by 3 matrix'.
Inertia tensor at full mass of the aircraft.
Empty inertia matrix - inertia tensor at mass without fuel
[0.5 0.0 0.0 0.0; 0.0 0.0 0.5 0.0; 0.0 0.0 0.5] (by default) | `a 3 by 3 matrix'.
Inertia tensor at aircraft mass without fuel.