public CoLqueryData liftQuery(Vector3 refVector)
{
CoLqueryData qry = new CoLqueryData();
Vector3 testVelocity = refVector;
speed = testVelocity.magnitude;
float angleOfAttackRad = 0f;
if (liftTransform != null)
{
angleOfAttackRad = CalculateAoA(liftTransform, testVelocity);
}
float liftCoeff = 2f * Mathf.PI * angleOfAttackRad;
lift = 0.5f * liftCoeff * airDensity * (speed * speed) * wingArea;
float aspectRatio = (span * span) / wingArea;
float dragCoeff = zeroLiftDrag + (liftCoeff * liftCoeff) / (Mathf.PI * aspectRatio * efficiency);
drag = 0.5f * dragCoeff * airDensity * (speed * speed) * wingArea;
lift *= power;
drag *= power;
qry.pos += liftTransform.position;
qry.dir += -liftTransform.up * lift;
qry.lift += qry.dir.magnitude;
//qry.dir.Normalize();
return(qry);
}
public void OnCenterOfLiftQuery(CenterOfLiftQuery qry)
{
if (moduleID == 0)
{
CoLqueryData queryData = new CoLqueryData();
queryData.refVector = qry.refVector;
for (int i = 0; i < liftSurfaces.Count; i++)
{
CoLqueryData newQuery = liftSurfaces[i].liftQuery(queryData.refVector);
float influence = new Vector2(queryData.dir.magnitude, newQuery.dir.magnitude).normalized.y;
queryData.pos = Vector3.Lerp(queryData.pos, newQuery.pos, influence);
queryData.lift += newQuery.lift;
queryData.dir = Vector3.Lerp(queryData.dir, newQuery.dir, influence);
}
queryData.dir.Normalize();
qry.dir = queryData.dir;
qry.lift = queryData.lift;
qry.pos = queryData.pos;
}
}
public void OnCenterOfLiftQuery(CenterOfLiftQuery qry)
{
if (moduleID == 0)
{
CoLqueryData queryData = new CoLqueryData();
queryData.refVector = qry.refVector;
for (int i = 0; i < liftSurfaces.Count; i++)
{
CoLqueryData newQuery = liftSurfaces[i].liftQuery(queryData.refVector);
float influence = new Vector2(queryData.dir.magnitude, newQuery.dir.magnitude).normalized.y;
queryData.pos = Vector3.Lerp(queryData.pos, newQuery.pos, influence);
queryData.lift += newQuery.lift;
queryData.dir = Vector3.Lerp(queryData.dir, newQuery.dir, influence);
}
queryData.dir.Normalize();
qry.dir = queryData.dir;
qry.lift = queryData.lift;
qry.pos = queryData.pos;
}
}
public CoLqueryData liftQuery(Vector3 refVector)
{
CoLqueryData qry = new CoLqueryData();
Vector3 testVelocity = refVector;
speed = testVelocity.magnitude;
float angleOfAttackRad = 0f;
if (liftTransform != null)
angleOfAttackRad = CalculateAoA(liftTransform, testVelocity);
float liftCoeff = 2f * Mathf.PI * angleOfAttackRad;
lift = 0.5f * liftCoeff * airDensity * (speed * speed) * wingArea;
float aspectRatio = (span * span) / wingArea;
float dragCoeff = zeroLiftDrag + (liftCoeff * liftCoeff) / (Mathf.PI * aspectRatio * efficiency);
drag = 0.5f * dragCoeff * airDensity * (speed * speed) * wingArea;
lift *= power;
drag *= power;
qry.pos += liftTransform.position;
qry.dir += -liftTransform.up * lift;
qry.lift += qry.dir.magnitude;
//qry.dir.Normalize();
return qry;
}
