public bool CalculateHoverThrust(List <IMyTerminalBlock> thrusters, out float atmoPercent, out float hydroPercent, out float ionPercent)
{
atmoPercent = 0;
hydroPercent = 0;
ionPercent = 0;
double ionThrust = calculateMaxThrust(thrusters, thrustion);
double atmoThrust = calculateMaxThrust(thrusters, thrustatmo);
double hydroThrust = calculateMaxThrust(thrusters, thrusthydro);
double physicalMass = _wicoBlockMaster.GetAllPhysicalMass();
Vector3D vGrav = _wicoBlockMaster.GetNaturalGravity();
double dGravity = vGrav.Length() / 9.81;
double hoverthrust = physicalMass * dGravity * 9.810;
if (atmoThrust > 0)
{
if (atmoThrust < hoverthrust)
{
atmoPercent = 100;
hoverthrust -= atmoThrust;
}
else
{
atmoPercent = (float)(hoverthrust / atmoThrust * 100);
if (atmoPercent > 0)
{
hoverthrust -= (atmoThrust * atmoPercent / 100);
}
}
}
if (hoverthrust < 0.01)
{
hoverthrust = 0;
}
// Echo("ALeft over thrust=" + hoverthrust.ToString("N0"));
if (ionThrust > 0 && hoverthrust > 0)
{
if (ionThrust < hoverthrust)
{
ionPercent = 100;
hoverthrust -= ionThrust;
}
else
{
ionPercent = (float)(hoverthrust / ionThrust * 100);
if (ionPercent > 0)
{
hoverthrust -= ((ionThrust * ionPercent) / 100);
}
}
}
if (hoverthrust < 0.01)
{
hoverthrust = 0;
}
// Echo("ILeft over thrust=" + hoverthrust.ToString("N0"));
if (hydroThrust > 0 && hoverthrust > 0)
{
if (hydroThrust < hoverthrust)
{
hydroPercent = 100;
hoverthrust -= hydroThrust;
}
else
{
hydroPercent = (float)(hoverthrust / hydroThrust * 100);
if (hydroPercent > 0)
{
hoverthrust -= ((hydroThrust * hydroPercent) / 100);
}
;
}
}
if (atmoPercent < 0.01)
{
atmoPercent = 0;
}
if (hydroPercent < 0.01)
{
hydroPercent = 0;
}
if (ionPercent < 0.01)
{
ionPercent = 0;
}
if (hoverthrust > 0)
{
return(false);
}
return(true);
}