Addition of the computation of aerodynamic derivatives

[florentLutz]

This PR is based on the work of @hugogarcia06 on the computation of the lateral aerodynamic derivatives. Here is a few remarks on their use:

• Some of these coefficients depend on lifting surface dihedral and twist angle. They have been added as inputs but they are only used in those components for now (no effects on the longitudinal derivatives).
• Some of these components depends on the flight conditions. It reuse the approach and cruise mach when applicable but sometimes they depend on the CG and AoA. For the CG a mid point between the aft and fwd position was taken but for the AoA it was added as an input.
• Theses coefficients are computed using the convention from Roskam meaning that for the lateral derivatives, the reference length is the wing span. Also, for the derivatives with respect to the rotationnal speed, said speed are made dimensionless by multiplying them by the reference length (MAC or span depending on the speed) and dividing them by two times the airspeed.

This PR also fixes #181 and closes #186

[codecov-commenter]

Codecov Report

Merging #185 (e2dfa72) into main (2ba9bc0) will increase coverage by 1.58%. The diff coverage is 95.09%.

@@            Coverage Diff             @@
##             main     #185      +/-   ##
==========================================
+ Coverage   83.42%   85.00%   +1.58%     
==========================================
  Files         317      365      +48     
  Lines       22806    26067    +3261     
  Branches     1362     1421      +59     
==========================================
+ Hits        19025    22158    +3133     
- Misses       3506     3603      +97     
- Partials      275      306      +31     

Impacted Files	Coverage Δ
...tga/models/aerodynamics/aerodynamics_high_speed.py	26.08% <0.00%> (-1.83%)	:arrow_down:
...ga/models/aerodynamics/components/elevator_aero.py	100.00% <ø> (ø)
...ga/models/aerodynamics/external/openvsp/openvsp.py	5.49% <0.00%> (-0.11%)	:arrow_down:
src/fastga/models/aerodynamics/external/vlm/vlm.py	8.10% <0.00%> (-0.18%)	:arrow_down:
...weight/mass_breakdown/a_airframe/a1_wing_weight.py	100.00% <ø> (ø)
...stga/models/aerodynamics/aerodynamics_low_speed.py	25.00% <25.00%> (-2.50%)	:arrow_down:
...ry/geom_components/ht/components/compute_ht_mac.py	53.22% <25.00%> (-0.38%)	:arrow_down:
...aerodynamics/aerodynamics_stability_derivatives.py	32.35% <32.35%> (ø)
.../fuel_propulsion/basicTurbo_prop/basicTP_engine.py	83.08% <50.00%> (-0.03%)	:arrow_down:
...a/models/aerodynamics/components/high_lift_aero.py	83.85% <66.66%> (-0.09%)	:arrow_down:
... and 104 more

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[florentLutz]

Added a commit that closes #186

[florentLutz]

Left to be done:

• [x] Change the location of the reference point for lateral derivatives
• [x] Have two separate variables for the reference AoA for high speed and low speed
• [x] Isolate derivatives that are not used in the sizing and put them in a separate module to save time
• [x] Solve Codacy issues