void FixedUpdate()
{
if (use_climo)
{
//Retrieve climatological data
kwind = _kwx_climo.get3DWind();
vel_list = _kwx_climo.getAero();
wx_list3d = _kwx_climo.getWx3D();
wx_list2d = _kwx_climo.getWx2D();
}
else if (use_point)
{
//Retrieve point forecast data
lsite = Util.get_last_lsite_short();
kwind = _kwx_point.get3DWind();
vel_list = _kwx_point.getAero();
wx_list3d = _kwx_point.getWx3D();
wx_list2d = _kwx_point.getWx2D();
}
//Check to see if outside of Kerbin's SOI
if (((FlightGlobals.ActiveVessel.mainBody != kerbin)))
{
Util.Log("Destroy toolbar as we're outside Kerbin's SOI");
//Don't display toolbar button or GUI when out of Kerbin SOI
ToolbarButtonOnFalse();
Destroy();
gui_removed = true;
}
else
{
//If we're back in Kerbin's SOI add the toolbar button and enable GUI oncemore.
if (gui_removed)
{
Util.Log("Re-add toolbar as we're back in Kerbin's SOI");
AddToolbarButton();
gui_removed = false;
}
}
aero_sdata = GetAeroStats();
}
Util.aero_stats GetAeroStats()
{
//Get current vessel
Vessel v = FlightGlobals.ActiveVessel;
Util.aero_stats aero_data = new Util.aero_stats();
Vector3d nVel = v.srf_velocity.normalized; //normalized velocity
double alpha = Vector3d.Dot(v.transform.forward, nVel);
alpha = Math.Asin(alpha) * RAD2DEG; // angle of attack re: velocity
double sideslip = Vector3d.Dot(v.transform.up, Vector3d.Exclude(v.transform.forward, nVel).normalized);
sideslip = Math.Acos(sideslip) * RAD2DEG; // sideslip re: velocity
if (double.IsNaN(sideslip))
{
sideslip = 0;
}
if (sideslip < 0)
{
sideslip = 180 + sideslip;
}
double shockTemp = v.externalTemperature; //External (air) temperature
//Get current vessel
Vector3d vLift = Vector3d.zero; // the sum of lift from all parts
Vector3d vDrag = Vector3d.zero; // the sum of drag from all parts
double sqrMag = v.srf_velocity.sqrMagnitude; //Square magnitude of vessel surface velocity
double Q = 0.5 * v.atmDensity * sqrMag; // dynamic pressure, aka Q
// i.e. your airspeed at sea level with the same Q
double soundSpeed = v.speedOfSound; //Speed of sound (m/s)
double mach = v.mach;
// Loop through all parts, checking modules in each part, to get sum of drag and lift.
for (int i = 0; i < v.Parts.Count; ++i)
{
Part p = v.Parts[i];
// get part drag (but not wing/surface drag)
vDrag += -p.dragVectorDir * p.dragScalar;
if (!p.hasLiftModule)
{
//Get body lift
Vector3 bodyLift = p.transform.rotation * (p.bodyLiftScalar * p.DragCubes.LiftForce);
bodyLift = Vector3.ProjectOnPlane(bodyLift, -p.dragVectorDir);
vLift += bodyLift;
}
// now find modules
for (int j = 0; j < p.Modules.Count; ++j)
{
var m = p.Modules[j];
if (m is ModuleLiftingSurface) // control surface derives from this
{
//Retrieve wind lift/drag
ModuleLiftingSurface wing = (ModuleLiftingSurface)m;
vLift += wing.liftForce;
vDrag += wing.dragForce;
}
}
}
Vector3d force = vLift + vDrag; // sum of all forces on the craft
Vector3d liftDir = -Vector3d.Cross(v.transform.right, nVel); // we need the "lift" direction, which
// is "up" from our current velocity vector and roll angle.
// Now we can compute the dots.
double lift = Vector3d.Dot(force, liftDir); // just the force in the 'lift' direction
double drag = Vector3d.Dot(force, -nVel); // drag force, = pDrag + lift-induced drag
double ldRatio = lift / drag; // Lift / Drag ratio
aero_data.alpha = alpha;
aero_data.sideslip = sideslip;
aero_data.soundSpeed = soundSpeed;
aero_data.mach = mach;
aero_data.Q = Q;
aero_data.lift = lift;
aero_data.drag = drag;
aero_data.ldRatio = ldRatio;
aero_data.shockTemp = shockTemp;
return(aero_data);
}