Estimate Center of Gravity
Calculating the position of the centre of gravity.
blockType: SubSystem
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Description
The Estimate Centre of Gravity block calculates the position of the centre of gravity as a function of mass and the rate of change of the centre of gravity position as a linear function of the rate of change of mass. Linear interpolation is used to determine the position of the centre of gravity.
Ports
Input
mass - mass
scalar
Mass.
Data types: Float64.
dm/dt - rate of change of mass
scalar
Rate of change of mass.
Data types: Float64.
Output
CG - position of centre of gravity
`vector 3 to 1
Coordinates of the centre of gravity of the aircraft.
Data types: Float64.
dCG/dt - rate of change of centre of gravity position
`vector 3 to 1
Components of the velocity of change of the position of the centre of gravity of the aircraft.
Data types: Float64.
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 centre of gravity - position of the centre of gravity at full mass
[1.0, 1.0, 1.0] (by default) | vector 3 to 1
Coordinates of the aircraft centre of gravity at full aircraft mass.
Empty centre of gravity - position of the centre of gravity at mass without fuel
[0.5, 0.5, 0.5] (by default) | vector 3 to 1
Coordinates of the aircraft centre of gravity at mass without fuel.