Code development platform for open source projects from the European Union institutions

Skip to content
Snippets Groups Projects
Commit a59c7f30 authored by Markus Quaritsch's avatar Markus Quaritsch
Browse files

Merge pull request #82 in VECTO/vecto-sim from...

Merge pull request #82 in VECTO/vecto-sim from ~EMQUARIMA/vecto-sim:feature/VECTO-123-airdrag-computation-and-writing to develop

* commit 'dc5845d5':
  remove interpolation table of delta-Cd(beta) and use polynomial function; testcases adapted
parents e55e728e dc5845d5
No related branches found
No related tags found
No related merge requests found
......@@ -265,36 +265,25 @@ namespace TUGraz.VectoCore.Models.SimulationComponent.Impl
protected Point[] CalculateAirResistanceCurve(AirDrag.AirDragEntry values)
{
// todo: get from vehicle or move whole procedure to vehicle
var cdA0Actual = _data.AerodynamicDragAera;
var betaValues = new Dictionary<int, SquareMeter>();
for (var beta = 0; beta <= 12; beta++) {
var deltaCdA = values.A1 * beta + values.A2 * beta * beta + values.A3 * beta * beta * beta;
betaValues[beta] = deltaCdA.SI<SquareMeter>();
}
var points = new List<Point> { new Point { X = 0.SI<MeterPerSecond>(), Y = 0.SI<SquareMeter>() } };
for (var vVeh = 60.KMPHtoMeterPerSecond();
vVeh.IsSmallerOrEqual(100.KMPHtoMeterPerSecond());
vVeh += 5.KMPHtoMeterPerSecond()) {
for (var speed = 60; speed <= 100; speed += 5) {
var vVeh = speed.KMPHtoMeterPerSecond();
var cdASum = 0.0.SI<SquareMeter>();
for (var alpha = 0; alpha <= 180; alpha += 10) {
var vWindX = Physics.BaseWindSpeed * Math.Cos(alpha.ToRadian());
var vWindY = Physics.BaseWindSpeed * Math.Sin(alpha.ToRadian());
var vAirX = vVeh + vWindX;
var vAirY = vWindY;
var vAir = VectoMath.Sqrt<MeterPerSecond>(vAirX * vAirX + vAirY * vAirY);
// var vAir = VectoMath.Sqrt<MeterPerSecond>(vAirX * vAirX + vAirY * vAirY);
var beta = Math.Atan((vAirY / vAirX).Value()).ToDegree();
var sec = betaValues.GetSection(b => b.Key < beta);
var deltaCdA = VectoMath.Interpolate(sec.Item1.Key, sec.Item2.Key, sec.Item1.Value, sec.Item2.Value, beta);
var cdA = cdA0Actual + deltaCdA;
var deltaCdA = ComputeDeltaCd(beta, values);
var cdA = _data.AerodynamicDragAera + deltaCdA;
var degreeShare = ((alpha != 0 && alpha != 180) ? 10.0 / 180.0 : 5.0 / 180.0);
cdASum += degreeShare * cdA * (vAir * vAir / (vVeh * vVeh)).Cast<Scalar>();
// cdASum += degreeShare * cdA * (vAir * vAir / (vVeh * vVeh)).Cast<Scalar>();
cdASum += degreeShare * cdA * ((vAirX * vAirX + vAirY * vAirY) / (vVeh * vVeh)).Cast<Scalar>();
}
points.Add(new Point { X = vVeh, Y = cdASum });
}
......@@ -303,6 +292,10 @@ namespace TUGraz.VectoCore.Models.SimulationComponent.Impl
return points.ToArray();
}
protected SquareMeter ComputeDeltaCd(double beta, AirDrag.AirDragEntry values)
{
return (values.A1 * beta + values.A2 * beta * beta + values.A3 * beta * beta * beta).SI<SquareMeter>();
}
public class VehicleState
{
......
......@@ -45,7 +45,7 @@ namespace TUGraz.VectoCore.Tests.Models.SimulationComponent
var retVal = requestPort.Request(absTime, dt, accell, gradient);
Assert.AreEqual(-2428.0412094587, mockPort.Force.Value(), 0.0001);
Assert.AreEqual(-2428.0205, mockPort.Force.Value(), 0.0001);
Assert.AreEqual(16.954303841, mockPort.Velocity.Value(), 0.0001);
}
......@@ -70,19 +70,19 @@ namespace TUGraz.VectoCore.Tests.Models.SimulationComponent
Assert.AreEqual(8.12204, tmp.Value(), Tolerance);
tmp = vehicle.ComputeEffectiveAirDragArea(75.KMPHtoMeterPerSecond());
Assert.AreEqual(7.67232, tmp.Value(), Tolerance);
Assert.AreEqual(7.67058, tmp.Value(), Tolerance);
tmp = vehicle.ComputeEffectiveAirDragArea(100.KMPHtoMeterPerSecond());
Assert.AreEqual(7.23949, tmp.Value(), Tolerance);
Assert.AreEqual(7.23735, tmp.Value(), Tolerance);
tmp = vehicle.ComputeEffectiveAirDragArea(52.1234.KMPHtoMeterPerSecond());
Assert.AreEqual(8.12204, tmp.Value(), Tolerance);
Assert.AreEqual(8.12196, tmp.Value(), Tolerance);
tmp = vehicle.ComputeEffectiveAirDragArea(73.5432.KMPHtoMeterPerSecond());
Assert.AreEqual(7.70967, tmp.Value(), Tolerance);
Assert.AreEqual(7.70815, tmp.Value(), Tolerance);
tmp = vehicle.ComputeEffectiveAirDragArea(92.8765.KMPHtoMeterPerSecond());
Assert.AreEqual(7.33617, tmp.Value(), Tolerance);
Assert.AreEqual(7.33443, tmp.Value(), Tolerance);
// ====================
......@@ -90,24 +90,24 @@ namespace TUGraz.VectoCore.Tests.Models.SimulationComponent
vehicle.Initialize(60.KMPHtoMeterPerSecond(), 0.SI<Radian>());
var avgForce = vehicle.AirDragResistance(0.SI<MeterPerSquareSecond>(), dt);
Assert.AreEqual(1340.13618774784, avgForce.Value(), Tolerance);
Assert.AreEqual(1340.12357, avgForce.Value(), Tolerance);
avgForce = vehicle.AirDragResistance(1.SI<MeterPerSquareSecond>(), dt);
Assert.AreEqual(1375.658146, avgForce.Value(), Tolerance);
Assert.AreEqual(1375.63226, avgForce.Value(), Tolerance);
avgForce = vehicle.AirDragResistance(0.5.SI<MeterPerSquareSecond>(), dt);
Assert.AreEqual(1357.785735, avgForce.Value(), Tolerance);
Assert.AreEqual(1357.76658, avgForce.Value(), Tolerance);
// - - - - - -
vehicle.Initialize(72.KMPHtoMeterPerSecond(), 0.SI<Radian>());
avgForce = vehicle.AirDragResistance(0.5.SI<MeterPerSquareSecond>(), dt);
Assert.AreEqual(1861.603488, avgForce.Value(), Tolerance);
Assert.AreEqual(1861.2734, avgForce.Value(), Tolerance);
dt = 3.SI<Second>();
avgForce = vehicle.AirDragResistance(1.SI<MeterPerSquareSecond>(), dt);
Assert.AreEqual(2102.13153, avgForce.Value(), Tolerance);
Assert.AreEqual(2101.63000, avgForce.Value(), Tolerance);
}
[TestMethod]
......@@ -133,11 +133,11 @@ namespace TUGraz.VectoCore.Tests.Models.SimulationComponent
var retVal = vehicle.Request(absTime, dt, 0.SI<MeterPerSquareSecond>(), 0.SI<Radian>());
vehicle.CommitSimulationStep(writer);
Assert.AreEqual(48213.70, ((SI)writer[ModalResultField.Pair]).Value(), 0.1);
Assert.AreEqual(48201.2777, ((SI)writer[ModalResultField.Pair]).Value(), 0.1);
retVal = vehicle.Request(absTime, dt, 1.SI<MeterPerSquareSecond>(), 0.SI<Radian>());
vehicle.CommitSimulationStep(writer);
Assert.AreEqual(49747.8535, ((SI)writer[ModalResultField.Pair]).Value(), 0.1);
Assert.AreEqual(49735.26379, ((SI)writer[ModalResultField.Pair]).Value(), 0.1);
}
}
}
\ No newline at end of file
0% Loading or .
You are about to add 0 people to the discussion. Proceed with caution.
Finish editing this message first!
Please register or to comment