/// <summary>
/// Updates the details by recalculating if requested.
/// </summary>
public void Update()
{
try
{
if (!this.hasCheckedAeroMods)
{
this.CheckAeroMods();
}
if (FlightGlobals.ActiveVessel.atmDensity < double.Epsilon || NearInstalled)
{
ShowDetails = false;
return;
}
ShowDetails = true;
if (FarInstalled)
{
TerminalVelocity = (double)this.farTerminalVelocity.Invoke(null, null);
}
else
{
var m = FlightGlobals.ActiveVessel.parts.Sum(part => PartExtensions.GetWetMass(part)) * 1000.0;
var g = FlightGlobals.getGeeForceAtPosition(FlightGlobals.ship_position).magnitude;
var a = FlightGlobals.ActiveVessel.parts.Sum(part => part.DragCubes.AreaDrag) * PhysicsGlobals.DragCubeMultiplier;
var p = FlightGlobals.ActiveVessel.atmDensity;
var c = PhysicsGlobals.DragMultiplier;
TerminalVelocity = Math.Sqrt((2.0 * m * g) / (p * a * c));
StaticPressure = FlightGlobals.ActiveVessel.staticPressurekPa;
DynamicPressure = FlightGlobals.ActiveVessel.dynamicPressurekPa;
}
Efficiency = FlightGlobals.ship_srfSpeed / TerminalVelocity;
}
catch (Exception ex)
{
MyLogger.Exception(ex, "AtmosphericProcessor->Update");
}
}
private void SetMassItems()
{
if (selectedPart.physicalSignificance == Part.PhysicalSignificance.FULL)
{
infoItems.Add(PartInfoItem.Create("Mass", Units.ToMass(PartExtensions.GetDryMass(selectedPart), PartExtensions.GetWetMass(selectedPart))));
}
}