public void Update(Mesh mesh)
{
Wing.UpdateSections();
Fuselage.UpdateSections();
HorizontalStabilizer.UpdateSections();
VerticalStabilizer.UpdateSections();
UnderCarriage.UpdateSections();
}
public Aircraft()
{
Fuselage = new Fuselage();
HorizontalStabilizer = new HorizontalStabilizer();
Wing = new Wing();
VerticalStabilizer = new VerticalStabilizer();
UnderCarriage = new UnderCarriage();
SeatsAcross = 10;
}
public void Generate(Mesh mesh)
{
Update(mesh);
Wing.Generate(mesh, new Vector2(0.15f, 0));
Wing.Engines.ForEach(x => x.Generate(mesh, new Vector2(0.25f, 0)));
Wing.Flaps.Generate(mesh, new Vector2(0.35f, 0));
Fuselage.Generate(mesh, Vector2.zero);
HorizontalStabilizer.Generate(mesh, new Vector2(0.45f, 0));
VerticalStabilizer.Generate(mesh, new Vector2(0.55f, 0));
UnderCarriage.Generate(mesh, new Vector2(0.65f, 0));
}
public void UpdateTailArea()
{
var l_v = ((Fuselage.Diameter * Fuselage.Afterbody.AfterbodyLengthDiameterRatio) + Fuselage.CentreFuselage.Length) - CentreOfGravity.z;
VerticalStabilizer.UpdateArea(Wing.Area, l_v, Wing.Span);
}