Engee documentation

Estimate Center of Gravity

Calculating the position of the centre of gravity.

estimate center of gravity

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.