void sumForces(List <PartModule> moduleList, Transform refTransform,
ref Vector3 translation, ref Vector3 torque)
{
List <PartModule> .Enumerator em = moduleList.GetEnumerator();
while (em.MoveNext())
{
PartModule mod = em.Current;
if (mod == null)
{
continue;
}
ModuleForces mf = mod.GetComponent <ModuleForces> ();
if (mf == null || !mf.enabled)
{
continue;
}
for (int t = 0; t < mf.vectors.Length; t++)
{
Vector3 force = -1 * mf.vectors [t].value; /* vectors represent exhaust force,
* so -1 for actual thrust */
translation += force;
torque += calcTorque(mf.vectors [t].transform, refTransform, force);
}
}
}
void calcRCSIsp(ref float num, ref float den)
{
foreach (PartModule pm in RCSBuildAid.RCS)
{
if (pm == null)
{
continue;
}
ModuleForces forces = pm.GetComponent <ModuleForces> ();
if (forces && forces.enabled)
{
ModuleRCS mod = (ModuleRCS)pm;
float v1 = mod.atmosphereCurve.Evaluate(0f);
foreach (VectorGraphic vector in forces.vectors)
{
Vector3 thrust = vector.value;
float v2 = Vector3.Dot(v1 * thrust.normalized,
RCSBuildAid.VesselForces.Thrust().normalized * -1);
/* calculating weighted mean, RCS thrust magnitude is already "weighted" */
num += thrust.magnitude * v2;
den += thrust.magnitude;
}
}
}
}
void addForcesSelection()
{
/* add force MonoBehaviours to parts grabbed by the cursor */
Profiler.BeginSample("[RCSBA] RCSBuildAid addForcesSelection");
if (EditorLogic.SelectedPart == null)
{
Profiler.EndSample();
return;
}
const bool onlyConnected = false;
var list = EditorUtils.GetSelectedModulesOf <ModuleRCS>(onlyConnected);
foreach (var pm in list)
{
ModuleForces.Add <RCSForce>(pm);
}
var moduleEngineList = EditorUtils.GetSelectedModulesOf <ModuleEngines>(onlyConnected);
var multiModeEngineList = EditorUtils.GetSelectedModulesOf <MultiModeEngine>(onlyConnected);
list = sortEngineList(moduleEngineList, multiModeEngineList);
foreach (var pm in list)
{
if (pm is MultiModeEngine)
{
ModuleForces.Add <MultiModeEngineForce>(pm);
}
else if (pm is ModuleEngines)
{
ModuleForces.Add <EngineForce>(pm);
}
}
Profiler.EndSample();
}
void sumForces(IList <ModuleForces> forceList, Transform refTransform, ref Vector3 translation, ref Vector3 torque)
{
for (int i = forceList.Count - 1; i >= 0; i--)
{
ModuleForces mforces = forceList [i];
Debug.Assert(mforces != null, "[RCSBA, MarkerForces]: ModuleForces != null");
if (!mforces.enabled)
{
continue;
}
for (int t = mforces.vectors.Length - 1; t >= 0; t--)
{
/* vectors represent exhaust force, so negative for actual thrust */
Vector3 force = -1 * mforces.vectors [t].value;
translation += force;
torque += calcTorque(mforces.vectors [t].transform, refTransform, force);
}
}
}
void addForces()
{
/* add force MonoBehaviours to parts in vessel */
Profiler.BeginSample("[RCSBA] RCSBuildAid addForces");
foreach (var mod in rcsList)
{
ModuleForces.Add <RCSForce> (mod);
}
foreach (var mod in engineList)
{
if (mod is ModuleEngines)
{
ModuleForces.Add <EngineForce>(mod);
}
else if (mod is MultiModeEngine)
{
ModuleForces.Add <MultiModeEngineForce> (mod);
}
}
Profiler.EndSample();
}
void sumForces(List <PartModule> moduleList, Transform refTransform,
ref Vector3 translation, ref Vector3 torque)
{
for (int i = 0; i < moduleList.Count; i++)
{
PartModule mod = moduleList [i];
if (mod == null)
{
continue;
}
ModuleForces mf = mod.GetComponent <ModuleForces> ();
if (mf == null || !mf.enabled)
{
continue;
}
for (int t = 0; t < mf.vectors.Length; t++)
{
/* vectors represent exhaust force, so -1 for actual thrust */
Vector3 force = -1 * mf.vectors [t].value;
translation += force;
torque += calcTorque(mf.vectors [t].transform, refTransform, force);
}
}
}
void onLeavingEditor()
{
ModuleForces.ClearLists();
}