When setting the mission name, the corresponding mission gets added to the MATLAB path, while others are removed.

To disable this, set 'changeMatlabPath' to false during creation of the mission

- Updated parachute data and masses

- Updated fins with new design constraint
- Updated aerodynamic coefficients for new fins

- Matrices updated wrt HRER_OPT_2_Venturi
- Fins optimisation performed

The merge method was made to merge two different Settings classes
The read method can read from any struct

Marcodagostino2 authored 5 months ago and Marco Luigi Gaibotti committed 4 months ago

Gravity model use a point-mass gravitation model
with an Earth radius defined in the Environment
class.

Marcodagostino2 authored 5 months ago and Marco Luigi Gaibotti committed 4 months ago

Added variable earth's radius in accordance with
the position on the earth's ellipsoid. Updated the model in
g computation.

to a bug in stability analysis

Stability analysis issue when using gaussian distribution for bounded ramp/terrain altitutes.
The first element of wind parameters must be with a uniform distribution. If you want to add
a gaussian distribution of wind parameters related to terrain wind, add a new altitude element.

[design-updates] Updated EuRoC simulations motors (smooth curve) for further comparison and added engine data like Roccaraso for post process compatibility

Thrust curve obtained through CC pressure data