public void OnPostAutopilotUpdate(FlightCtrlState s)
{
if (!Valid || !CFG.Enabled)
{
return;
}
//handle engines
VSL.PostUpdateState(s);
VSL.Engines.Tune();
if (VSL.Engines.NumActive > 0)
{
//:preset manual limits for translation if needed
var translation = VSL.Controls.EnginesTranslation;
if (VSL.Controls.HasTranslation)
{
translation += VSL.Controls.Translation;
}
if (!translation.IsZero())
{
EngineOptimizer.PresetLimitsForTranslation(VSL.Engines.Active.Maneuver, translation.normalized);
if (CFG.VSCIsActive && !VSL.Controls.HasTranslation)
{
EngineOptimizer.LimitInDirection(VSL.Engines.Active.Maneuver, VSL.Physics.UpL);
}
}
ENG.Steer();
}
RCS.Steer();
VSL.Engines.SetControls();
VSL.FinalUpdate();
}
public bool OptimizeForZeroTorque(Vector3 MoI)
{
var torque = Vector3.zero;
float torque_error, angle_error, max_limit;
if (Balanced.Count > 0)
{
torque = TorqueProps.CalculateImbalance(true, Manual, UnBalanced);
EngineOptimizer.OptimizeLimitsForTorque(Balanced, Vector3.zero, torque, MoI, true,
out max_limit, out torque_error, out angle_error);
}
if (Steering.Count > 0)
{
torque = TorqueProps.CalculateImbalance(true, Manual, UnBalanced, Balanced);
return(EngineOptimizer.OptimizeLimitsForTorque(Steering, Vector3.zero, torque, MoI, true,
out max_limit, out torque_error, out angle_error));
}
return(true);
}
void UpdateShipStats()
{
MinLimit = 0;
var thrust = Vector3.zero;
var selected_parts = GetSelectedParts();
CalculateMassAndCoM(selected_parts);
if (CFG != null && CFG.Enabled && Engines.Count > 0)
{
ActiveEngines.Clear();
for (int i = 0, EnginesCount = Engines.Count; i < EnginesCount; i++)
{
var e = Engines[i];
var ecfg = CFG.ActiveProfile.GetConfig(e);
if (ecfg == null || ecfg.On)
{
ActiveEngines.Add(e);
}
}
if (selected_parts.Count > 0)
{
var selected_engines = new List <EngineWrapper>();
selected_parts.ForEach(p => find_engines_recursively(p, selected_engines));
ActiveEngines.AddRange(selected_engines);
}
if (ActiveEngines.Count > 0)
{
ActiveEngines.ForEach(process_active_engine);
compute_inertia_tensor();
selected_parts.ForEach(update_inertia_tensor);
ActiveEngines.SortByRole();
float max_limit, torque_error, angle_error;
var imbalance = TorqueProps.CalculateImbalance(true, ActiveEngines.Manual, ActiveEngines.UnBalanced);
if (ActiveEngines.Balanced.Count > 0)
{
EngineOptimizer.OptimizeLimitsForTorque(ActiveEngines.Balanced, Vector3.zero, imbalance, MoI, true,
out max_limit, out torque_error, out angle_error);
imbalance = TorqueProps.CalculateImbalance(true, ActiveEngines.Manual, ActiveEngines.UnBalanced, ActiveEngines.Balanced);
}
if (ActiveEngines.Steering.Count > 0)
{
if (!EngineOptimizer.OptimizeLimitsForTorque(ActiveEngines.Steering, Vector3.zero, imbalance, MoI, true,
out max_limit, out torque_error, out angle_error))
{
ActiveEngines.Steering.ForEach(e => e.limit = 0);
ActiveEngines.Balanced.ForEach(e => e.limit = 0);
}
}
MinLimit = 1;
for (int i = 0, ActiveEnginesCount = ActiveEngines.Count; i < ActiveEnginesCount; i++)
{
var e = ActiveEngines[i];
thrust += e.wThrustDir * e.nominalCurrentThrust(e.limit);
if (e.Role != TCARole.MANUAL &&
e.Role != TCARole.MANEUVER &&
MinLimit > e.limit)
{
MinLimit = e.limit;
}
e.forceThrustPercentage(e.limit * 100);
}
var T = thrust.magnitude / Utils.G0;
MinTWR = T / Mass;
MaxTWR = T / DryMass;
}
}
}