//public STKDataProvider(IAgStkObject object0,string Name, bool needPreData)
//{
// m_selectedObject = object0;
// m_providerGroup = m_selectedObject.DataProviders["Cartesian Velocity"] as IAgDataProviderGroup;
// IAgDataProvider CartVel_provider= (m_providerGroup.Group["J2000"] as IAgDataProvider);
// ///Cast Appropiate Data Pro
// IAgDataPrvTimeVar Velocity = CartVel_provider as IAgDataPrvTimeVar;
// Array elem = new object[] { "x" };
// IAgDrResult Speed = Velocity.ExecElements("19 May 2019 22:00:00.000", "19 May 2019 22:10:00.000", 60, ref elem );
// m_dataSe = Speed.DataSets[0].GetValues();
// ///update_Dataset(26667, "Name", speed);
// ///Console.WriteLine(CartVel_providers)
//}
public System.Array acquireDataset(string startTime, string stopTime, double timeStep)
{
IAgDataProvider provider = null;
if (m_parent != m_superParent)
{
m_providerGroup = m_StkObj.DataProviders[m_superParent] as IAgDataProviderGroup;
provider = (m_providerGroup.Group[m_parent] as IAgDataProvider); //m_parent
}
else if (m_parent == m_superParent)
{
provider = m_StkObj.DataProviders[m_parent] as IAgDataProvider;
}
///Cast Appropiate Data Pro
try
{
IAgDataPrvTimeVar Velocity = provider as IAgDataPrvTimeVar;
Array elem = new object[] { m_DP2 };
IAgDrResult result = Velocity.ExecElements(startTime, stopTime, timeStep, ref elem);
m_dataArray = result.DataSets[0].GetValues();
}
catch
{
IAgDataPrvInterval Velocity = provider as IAgDataPrvInterval;
if (Velocity != null)
{
Array elem = new object[] { m_DP2 };
IAgDrResult result = Velocity.ExecElements(startTime, stopTime, ref elem);
m_dataArray = result.DataSets[0].GetValues();
}
else
{
m_Error = true;
}
}
return(m_dataArray);
}
public List <Waypoint> RasterSearchWaypointGenerator(
string areaTargetPath, string heading, double speed, double altitude, double turnRadius,
SwathWidthType swathType, double swathParameter)
{
List <Waypoint> waypoints = new List <Waypoint>();
IAgStkObject areaTarget = root.GetObjectFromPath(areaTargetPath);
IAgAreaTarget areaTargetObj = (IAgAreaTarget)areaTarget;
bool areaTargetElActive = areaTarget.AccessConstraints.IsConstraintActive(AgEAccessConstraints.eCstrElevationAngle);
double restoreAngle = 0;
if (!areaTargetElActive)
{
IAgAccessCnstrAngle elevationMin = areaTarget.AccessConstraints.AddConstraint(AgEAccessConstraints.eCstrElevationAngle) as IAgAccessCnstrAngle;
root.UnitPreferences["Angle"].SetCurrentUnit("deg");
elevationMin.Angle = 90;
}
else
{
IAgAccessCnstrAngle elevationMin = areaTarget.AccessConstraints.GetActiveConstraint(AgEAccessConstraints.eCstrElevationAngle) as IAgAccessCnstrAngle;
root.UnitPreferences["Angle"].SetCurrentUnit("deg");
restoreAngle = (double)elevationMin.Angle;
elevationMin.Angle = 90;
}
double minLat = 90;
double maxLat = -90;
double minLon = 180;
double maxLon = -180;
root.UnitPreferences["Angle"].SetCurrentUnit("deg");
switch (areaTargetObj.AreaType)
{
case AgEAreaType.eEllipse:
IAgDataProviderGroup boundingProvider = areaTarget.DataProviders["Bounding Rectangle"] as IAgDataProviderGroup;
IAgDataPrvFixed dpElements = boundingProvider.Group["Corner Points"] as IAgDataPrvFixed;
IAgDrResult atDataPrvResult = dpElements.Exec();
Array atLats = atDataPrvResult.DataSets.GetDataSetByName("Geodetic-Lat").GetValues();
Array atLons = atDataPrvResult.DataSets.GetDataSetByName("Geodetic-Lon").GetValues();
foreach (object item in atLats)
{
if ((double)item > maxLat)
{
maxLat = (double)item;
}
if ((double)item < minLat)
{
minLat = (double)item;
}
}
foreach (object item in atLons)
{
if ((double)item > maxLon)
{
maxLon = (double)item;
}
if ((double)item < minLon)
{
minLon = (double)item;
}
}
break;
case AgEAreaType.ePattern:
IAgAreaTypePatternCollection boundary = areaTargetObj.AreaTypeData as IAgAreaTypePatternCollection;
foreach (IAgAreaTypePattern item in boundary)
{
if ((double)item.Lat > maxLat)
{
maxLat = (double)item.Lat;
}
if ((double)item.Lat < minLat)
{
minLat = (double)item.Lat;
}
if ((double)item.Lon > maxLon)
{
maxLon = (double)item.Lon;
}
if ((double)item.Lon < minLon)
{
minLon = (double)item.Lon;
}
}
break;
default:
break;
}
double deltaLat = maxLat - minLat;
double deltaLon = maxLon - minLon;
IAgExecCmdResult cmdResult;
switch (heading)
{
case "NorthSouth":
cmdResult = root.ExecuteCommand("MeasureSurfaceDistance * " +
minLat + " " + minLon + " " + minLat + " " + maxLon);
break;
case "EastWest":
cmdResult = root.ExecuteCommand("MeasureSurfaceDistance * " +
minLat + " " + minLon + " " + maxLat + " " + minLon);
break;
default:
cmdResult = root.ExecuteCommand("MeasureSurfaceDistance * " +
minLat + " " + minLon + " " + maxLat + " " + minLon);
break;
}
double regionWidth = double.Parse(cmdResult[0]);
int numPasses = DetermineNumPasses(swathType, swathParameter, altitude, regionWidth, null);
if (numPasses < 1)
{
MessageBox.Show("No Passes. Try Adjusting Swath Width Parameters");
return(waypoints);
}
root.BeginUpdate();
string gvName = uniqueName("gridTester", AgESTKObjectType.eGroundVehicle);
IAgGroundVehicle groundVehicle = root.CurrentScenario.Children.New(AgESTKObjectType.eGroundVehicle, gvName) as IAgGroundVehicle;
groundVehicle.Graphics.SetAttributesType(AgEVeGfxAttributes.eAttributesBasic);
IAgVeGfxAttributesBasic gvGfx = groundVehicle.Graphics.Attributes as IAgVeGfxAttributesBasic;
gvGfx.Inherit = false;
gvGfx.IsVisible = false;
IAgVePropagatorGreatArc route = groundVehicle.Route as IAgVePropagatorGreatArc;
//route.ArcGranularity = 51.333;
route.SetAltitudeRefType(AgEVeAltitudeRef.eWayPtAltRefWGS84);
route.Method = AgEVeWayPtCompMethod.eDetermineTimeAccFromVel;
Waypoint waypoint1 = new Waypoint();
Waypoint waypoint2 = new Waypoint();
bool headEast = true;
double loopMin;
double loopMax;
double gridAngleStep;
switch (heading)
{
case "NorthSouth":
loopMin = minLon;
loopMax = maxLon;
gridAngleStep = (maxLon - minLon) / numPasses;
break;
case "EastWest":
loopMin = minLat;
loopMax = maxLat;
gridAngleStep = (maxLat - minLat) / numPasses;
break;
default:
loopMin = minLat;
loopMax = maxLat;
gridAngleStep = .95 * (maxLat - minLat) / numPasses;
break;
}
for (double eval = loopMin; eval <= loopMax; eval += gridAngleStep)
{
route.Waypoints.RemoveAll();
IAgVeWaypointsElement thisWaypoint1;
IAgVeWaypointsElement thisWaypoint2;
switch (heading)
{
case "NorthSouth":
thisWaypoint1 = route.Waypoints.Add();
thisWaypoint1.Latitude = minLat - gridAngleStep;
thisWaypoint1.Longitude = eval;
thisWaypoint1.Altitude = 0;
thisWaypoint2 = route.Waypoints.Add();
thisWaypoint2.Latitude = maxLat + gridAngleStep;
thisWaypoint2.Longitude = eval;
thisWaypoint2.Altitude = 0;
break;
case "EastWest":
default:
thisWaypoint1 = route.Waypoints.Add();
thisWaypoint1.Latitude = eval;
thisWaypoint1.Longitude = minLon - gridAngleStep;
thisWaypoint1.Altitude = 0;
thisWaypoint2 = route.Waypoints.Add();
thisWaypoint2.Latitude = eval;
thisWaypoint2.Longitude = maxLon + gridAngleStep;
thisWaypoint2.Altitude = 0;
break;
}
route.Propagate();
IAgStkAccess access = areaTarget.GetAccessToObject((IAgStkObject)groundVehicle);
access.ComputeAccess();
IAgDataPrvInterval dpAccess = access.DataProviders["Access Data"] as IAgDataPrvInterval;
IAgScenario scen = root.CurrentScenario as IAgScenario;
IAgDrResult result = dpAccess.Exec(scen.StartTime, scen.StopTime);
if (result.DataSets.Count > 0)
{
Array startTimes = result.DataSets.GetDataSetByName("Start Time").GetValues();
Array stopTimes = result.DataSets.GetDataSetByName("Stop Time").GetValues();
string startTime = (string)startTimes.GetValue(0);
string stopTime = (string)stopTimes.GetValue(stopTimes.GetLength(0) - 1);
IAgDataProviderGroup dpLLA = ((IAgStkObject)groundVehicle).DataProviders["LLA State"] as IAgDataProviderGroup;
IAgDataPrvTimeVar dpElements = dpLLA.Group["Fixed"] as IAgDataPrvTimeVar;
IAgDrResult DataPrvResult = dpElements.ExecSingle(startTime);
Array Lats = DataPrvResult.DataSets.GetDataSetByName("Lat").GetValues();
Array Lons = DataPrvResult.DataSets.GetDataSetByName("Lon").GetValues();
waypoint1 = new Waypoint();
waypoint1.Latitude = (double)Lats.GetValue(0);
waypoint1.Longitude = (double)Lons.GetValue(0);
waypoint1.Altitude = altitude;
waypoint1.SurfaceAltitude = 0;
waypoint1.Speed = speed;
waypoint1.TurnRadius = turnRadius;
IAgDataProviderGroup dpLLA1 = ((IAgStkObject)groundVehicle).DataProviders["LLA State"] as IAgDataProviderGroup;
IAgDataPrvTimeVar dpElements1 = dpLLA1.Group["Fixed"] as IAgDataPrvTimeVar;
IAgDrResult DataPrvResult1 = dpElements1.ExecSingle(stopTime);
Array Lats1 = DataPrvResult1.DataSets.GetDataSetByName("Lat").GetValues();
Array Lons1 = DataPrvResult1.DataSets.GetDataSetByName("Lon").GetValues();
waypoint2 = new Waypoint();
waypoint2.Latitude = (double)Lats1.GetValue(0);
waypoint2.Longitude = (double)Lons1.GetValue(0);
waypoint2.Altitude = altitude;
waypoint2.SurfaceAltitude = 0;
waypoint2.Speed = speed;
waypoint2.TurnRadius = turnRadius;
if (headEast)
{
waypoints.Add(waypoint1);
waypoints.Add(waypoint2);
}
else
{
waypoints.Add(waypoint2);
waypoints.Add(waypoint1);
}
headEast = !headEast;
}
access.RemoveAccess();
}
((IAgStkObject)groundVehicle).Unload();
if (!areaTargetElActive)
{
areaTarget.AccessConstraints.RemoveConstraint(AgEAccessConstraints.eCstrElevationAngle);
}
else
{
IAgAccessCnstrAngle elevationMin = areaTarget.AccessConstraints.GetActiveConstraint(AgEAccessConstraints.eCstrElevationAngle) as IAgAccessCnstrAngle;
root.UnitPreferences["Angle"].SetCurrentUnit("deg");
elevationMin.Angle = restoreAngle;
}
root.EndUpdate();
root.UnitPreferences.ResetUnits();
return(waypoints);
}
//Main Function
private void Generate_Click(object sender, EventArgs e)
{
int check = FieldCheck();
if (check == 0)
{
RemoveProximityGeometry();
try
{
CommonData.StkRoot.UnitPreferences.SetCurrentUnit("Distance", "km");
CommonData.RunList.Clear();
CommonData.TargetName = TargetSat.Text;
CommonData.ActorName = ActorSat.Text;
//Set user bounds for safety
double userMinRange = Double.Parse(SphericalMag.Text) / 1000;
double userMinR = Double.Parse(RMag.Text) / 1000;
double userMinI = Double.Parse(IMag.Text) / 1000;
double userMinC = Double.Parse(CMag.Text) / 1000;
IAgScenario scenario = CommonData.StkRoot.CurrentScenario as IAgScenario;
IAgStkObject satObj = CommonData.StkRoot.GetObjectFromPath("Satellite/" + ActorSat.Text);
IAgSatellite sat = satObj as IAgSatellite;
//Get all maneuver end times for actor satellite
IAgDataProviderGroup maneuverDpGroup = satObj.DataProviders["Astrogator Maneuver Ephemeris Block Final"] as IAgDataProviderGroup;
IAgDataPrvTimeVar maneuverDp = maneuverDpGroup.Group["Cartesian Elems"] as IAgDataPrvTimeVar;
IAgDrResult result = maneuverDp.Exec(scenario.StartTime, scenario.StopTime, 60);
IAgDrDataSetCollection maneuverData = result.DataSets;
//If there is maneuvers, run iterations for each maneuver. If no maneuvers then just pull closest RIC data for entire trajectory
if (maneuverData.Count != 0)
{
CommonData.HasManeuvers = true;
//Get maneuver numbers
IAgDataPrvInterval summaryDp = satObj.DataProviders["Maneuver Summary"] as IAgDataPrvInterval;
IAgDrResult summaryResult = summaryDp.Exec(scenario.StartTime, scenario.StopTime);
Array maneuverNumbers = summaryResult.DataSets.GetDataSetByName("Maneuver Number").GetValues();
int maxManeuverNum = maneuverNumbers.Length;
//Get handles to cartesian position and velocity to seed passive safety runs
IAgDataProviderGroup cartPos = satObj.DataProviders["Cartesian Position"] as IAgDataProviderGroup;
IAgDataPrvTimeVar cartPosDP = cartPos.Group["ICRF"] as IAgDataPrvTimeVar;
IAgDataProviderGroup cartVel = satObj.DataProviders["Cartesian Velocity"] as IAgDataProviderGroup;
IAgDataPrvTimeVar cartVelDP = cartVel.Group["ICRF"] as IAgDataPrvTimeVar;
//Create passive safety satellite. Set to Astrogator and pull handles to initial state and propagate segments
IAgStkObject passiveSatObj = CreatorFunctions.GetCreateSatellite("PassiveCheck");
IAgSatellite passiveSat = passiveSatObj as IAgSatellite;
passiveSat.SetPropagatorType(AgEVePropagatorType.ePropagatorAstrogator);
IAgVADriverMCS passiveDriver = passiveSat.Propagator as IAgVADriverMCS;
IAgVAMCSInitialState intState = passiveDriver.MainSequence[0] as IAgVAMCSInitialState;
IAgVAMCSPropagate prop = passiveDriver.MainSequence[1] as IAgVAMCSPropagate;
IAgVAStoppingConditionElement sc1 = prop.StoppingConditions[0];
IAgVAStoppingCondition sc = sc1.Properties as IAgVAStoppingCondition;
sc.Trip = PropTime.Text;
AgVAElementCartesian element = intState.Element as AgVAElementCartesian;
Array epoch;
Array vx;
Array vy;
Array vz;
Array x;
Array y;
Array z;
String epochCur;
DateTime dateCur;
//Assign cartesian elements to PassiveCheck satellite from actor maneuver maneuver data. Run each iteration to see if resulting trajectory violates constraints
for (int i = 0; i < maxManeuverNum; i++)
{
//Get maneuver time and offset in time by 0.25 sec to account for boundrary conditions around impulsive maneuvers
epoch = maneuverData[0 + (i * 7)].GetValues();
epochCur = epoch.GetValue(0).ToString();
dateCur = DateTime.Parse(epochCur);
dateCur = dateCur.AddMilliseconds(250);
//dateCur = DateTime.ParseExact(epochCur, "dd MMM yyyy HH:mm:ss.fff", CultureInfo.InvariantCulture);
epochCur = dateCur.ToString("dd MMM yyyy HH:mm:ss.fff");
//Get cartesian state vector for given time
result = cartPosDP.ExecSingle(epochCur);
x = result.DataSets.GetDataSetByName("x").GetValues();
y = result.DataSets.GetDataSetByName("y").GetValues();
z = result.DataSets.GetDataSetByName("z").GetValues();
result = cartVelDP.ExecSingle(epochCur);
vx = result.DataSets.GetDataSetByName("x").GetValues();
vy = result.DataSets.GetDataSetByName("y").GetValues();
vz = result.DataSets.GetDataSetByName("z").GetValues();
//Create passive run output to be used in visualization
PassiveRun run = new PassiveRun();
run.UserMinRange = Double.Parse(SphericalMag.Text) / 1000;
run.UserMinR = Double.Parse(RMag.Text) / 1000;
run.UserMinI = Double.Parse(IMag.Text) / 1000;
run.UserMinC = Double.Parse(CMag.Text) / 1000;
intState.OrbitEpoch = epochCur;
element.Vx = Double.Parse(vx.GetValue(0).ToString());
element.Vy = Double.Parse(vy.GetValue(0).ToString());
element.Vz = Double.Parse(vz.GetValue(0).ToString());
element.X = Double.Parse(x.GetValue(0).ToString());
element.Y = Double.Parse(y.GetValue(0).ToString());
element.Z = Double.Parse(z.GetValue(0).ToString());
passiveDriver.RunMCS();
run.Vx = Double.Parse(vx.GetValue(0).ToString());
run.Vy = Double.Parse(vy.GetValue(0).ToString());
run.Vz = Double.Parse(vz.GetValue(0).ToString());
run.X = Double.Parse(x.GetValue(0).ToString());
run.Y = Double.Parse(y.GetValue(0).ToString());
run.Z = Double.Parse(z.GetValue(0).ToString());
run.PropTime = Double.Parse(PropTime.Text);
//Pull closest point to target for each iteration and save to passive run output
IAgDataProvider psatDp = passiveSatObj.DataProviders["RIC Coordinates"] as IAgDataProvider;
psatDp.PreData = "Satellite/" + TargetSat.Text;
IAgDataPrvTimeVar psatDpTimeVar = psatDp as IAgDataPrvTimeVar;
IAgDrResult psatDp2 = psatDpTimeVar.Exec(scenario.StartTime, scenario.StopTime, Double.Parse(TimeStep.Text));
run.Range = psatDp2.DataSets.GetDataSetByName("Range").GetValues();
run.Intrack = psatDp2.DataSets.GetDataSetByName("In-Track").GetValues();
run.Crosstrack = psatDp2.DataSets.GetDataSetByName("Cross-Track").GetValues();
run.Radial = psatDp2.DataSets.GetDataSetByName("Radial").GetValues();
run.MinRange = MathFunctions.ArrayMin(run.Range);
run.MinIntrack = MathFunctions.ArrayMinAbs(run.Intrack);
run.MinCrosstrack = MathFunctions.ArrayMinAbs(run.Crosstrack);
run.MinRadial = MathFunctions.ArrayMinAbs(run.Radial);
//run.ManeuverTime = epoch.GetValue(0).ToString();
run.ManeuverTime = epochCur;
//spherical
if (radioButton1.Checked)
{
run.IsSpherical = true;
if (run.MinRange < userMinRange)
{
run.Safe = false;
}
else
{
run.Safe = true;
}
}
//independent axis
else
{
run.IsSpherical = false;
if (Math.Abs(run.MinIntrack) < userMinI && Math.Abs(run.MinRadial) < userMinR && Math.Abs(run.MinCrosstrack) < userMinC)
{
bool tripped = false;
for (int j = 0; j < run.Range.Length; j++)
{
if (Math.Abs(Double.Parse(run.Intrack.GetValue(j).ToString())) < userMinI && Math.Abs(Double.Parse(run.Radial.GetValue(j).ToString())) < userMinR && Math.Abs(Double.Parse(run.Crosstrack.GetValue(j).ToString())) < userMinC)
{
run.Safe = false;
tripped = true;
break;
}
}
if (!tripped)
{
run.Safe = true;
}
}
else
{
run.Safe = true;
}
}
CommonData.RunList.Add(run);
}
}
else
{
CommonData.HasManeuvers = false;
PassiveRun run = new PassiveRun();
IAgDataProvider satDp = satObj.DataProviders["RIC Coordinates"] as IAgDataProvider;
satDp.PreData = "Satellite/" + TargetSat.Text;
IAgDataPrvTimeVar satDpTimeVar = satDp as IAgDataPrvTimeVar;
IAgDrResult satDp2 = satDpTimeVar.Exec(scenario.StartTime, scenario.StopTime, Double.Parse(TimeStep.Text));
run.Range = satDp2.DataSets.GetDataSetByName("Range").GetValues();
run.Intrack = satDp2.DataSets.GetDataSetByName("In-Track").GetValues();
run.Crosstrack = satDp2.DataSets.GetDataSetByName("Cross-Track").GetValues();
run.Radial = satDp2.DataSets.GetDataSetByName("Radial").GetValues();
run.MinRange = MathFunctions.ArrayMin(run.Range);
run.MinIntrack = MathFunctions.ArrayMinAbs(run.Intrack);
run.MinCrosstrack = MathFunctions.ArrayMinAbs(run.Crosstrack);
run.MinRadial = MathFunctions.ArrayMinAbs(run.Radial);
run.ManeuverTime = "N/A";
//spherical
if (radioButton1.Checked)
{
run.IsSpherical = true;
if (run.MinRange < userMinRange)
{
run.Safe = false;
}
else
{
run.Safe = true;
}
}
//independent axis
else
{
run.IsSpherical = false;
if (Math.Abs(run.MinIntrack) < userMinI && Math.Abs(run.MinRadial) < userMinR && Math.Abs(run.MinCrosstrack) < userMinC)
{
bool tripped = false;
for (int j = 0; j < run.Range.Length; j++)
{
if (Math.Abs(Double.Parse(run.Intrack.GetValue(j).ToString())) < userMinI && Math.Abs(Double.Parse(run.Radial.GetValue(j).ToString())) < userMinR && Math.Abs(Double.Parse(run.Crosstrack.GetValue(j).ToString())) < userMinC)
{
run.Safe = false;
tripped = true;
break;
}
}
if (!tripped)
{
run.Safe = true;
}
}
else
{
run.Safe = true;
}
}
CommonData.RunList.Add(run);
}
CommonData.BeenRun = true;
}
catch (Exception)
{
MessageBox.Show("Passive Safety Check Failed");
}
}
}
public void EstimateProbability()
{
StkAssistant.SetAnalysisIntervalFromTCA(this.Primary.EpochISOYMD);
string primaryPath = Primary.BaselineObjectPath;
string primaryType = Primary.BaselineObjectType;
string primaryName = primaryPath.Substring(primaryPath.LastIndexOf("/") + 1);
string secondaryPath = Secondary.BaselineObjectPath;
string secondaryName = secondaryPath.Substring(secondaryPath.LastIndexOf("/") + 1);
string catName = "CAT_" + primaryName;
int counter = 0;
while (StkAssistant.Root.CurrentScenario.Children.Contains(AgESTKObjectType.eAdvCat, catName))
{
catName = "CAT_" + primaryName + "_" + (++counter).ToString();
}
IAgStkObject cat = StkAssistant.Root.CurrentScenario.Children.New(AgESTKObjectType.eAdvCat, catName);
string cmdResult;
StkAssistant.TryConnect("Save / " + primaryPath, out cmdResult);
StkAssistant.TryConnect("Save / " + secondaryPath, out cmdResult);
StkAssistant.TryConnect("ACAT */AdvCAT/" + catName + " TimePeriod \"" + StkAssistant.Scenario.StartTime + "\" \"" + StkAssistant.Scenario.StopTime + "\"", out cmdResult);
StkAssistant.TryConnect("ACAT */AdvCAT/" + catName + " Primary Add \"" + primaryName + ".sa\" Cov", out cmdResult);
StkAssistant.TryConnect("ACAT */AdvCAT/" + catName + " Secondary Add \"" + secondaryName + ".sa\" Cov", out cmdResult);
StkAssistant.TryConnect("ACAT */AdvCAT/" + catName + " Compute ShowProgress On", out cmdResult);
StkAssistant.TryConnect("VO */AdvCAT/" + catName + " AdvCATAttributes ShowSecondary On ShowAllSecondary On", out cmdResult);
//StkAssistant.TryConnect("ReportCreate */AdvCAT/" + catName + " Type Display Style \"Close Approach By Min Range\"", out cmdResult);
StkAssistant.TryConnect("ACATEvents_RM */AdvCAT/" + catName, out cmdResult);
string catTCA;
if (!cmdResult.Equals("No events found."))
{
catTCA = cmdResult.Split(',')[5];
IAgStkObject catObject = StkAssistant.Root.GetObjectFromPath("*/AdvCAT/" + catName);
IAgDataPrvInterval catDP = cat.DataProviders["Events by Min Range"] as IAgDataPrvInterval;
IAgDrResult catResult = catDP.Exec(StkAssistant.Scenario.StartTime, StkAssistant.Scenario.StopTime);
double catMaxProb = (double)catResult.DataSets.GetDataSetByName("Max Collision Probability").GetValues().GetValue(0);
double catSigmaDilution = (double)catResult.DataSets.GetDataSetByName("Sigma Dilution Threshold").GetValues().GetValue(0);
if (Probability == 0)
{
Probability = catMaxProb;
}
if (SigmaDilution == 0)
{
SigmaDilution = Math.Round(catSigmaDilution, 3);
}
}
cat.Unload();
}
public Array GetDataProviders(string stkObjectPath, string DataProviderName,
string GroupName, string ElementName)
{
string startTime = scen.StartTime.ToString();
string stopTime = scen.StopTime.ToString();
double stepSize = 60;
IAgStkObject stkObject = root.GetObjectFromPath(stkObjectPath);
IAgDataProviderInfo dpInfo = stkObject.DataProviders[DataProviderName];
IAgDataProvider dataProvider = stkObject.DataProviders[DataProviderName] as IAgDataProvider;
if (dpInfo.IsGroup())
{
IAgDataProviderGroup dpGroup = dpInfo as IAgDataProviderGroup;
IAgDataProviders dpAvailable = dpGroup.Group;
for (int i = 0; i < dpAvailable.Count; ++i)
{
if (dpAvailable[i].Name == GroupName)
{
dataProvider = dpAvailable[i] as IAgDataProvider;
break;
}
}
}
IAgDrResult dpResult = null;
switch (dpInfo.Type)
{
case AgEDataProviderType.eDrFixed:
//Fixed data doesnt change over time
IAgDataPrvFixed dpFixed = dataProvider as IAgDataPrvFixed;
dpResult = dpFixed.Exec();
break;
case AgEDataProviderType.eDrIntvl:
//Interval data is given as a list of intervals with start, stop and duration
IAgDataPrvInterval dpInterval = dataProvider as IAgDataPrvInterval;
//Must provide analysis start and stop time
dpResult = dpInterval.Exec(startTime, stopTime);
break;
case AgEDataProviderType.eDrTimeVar:
//Time varyign data is given as an array of time based values
IAgDataPrvTimeVar dpTimeVarying = dataProvider as IAgDataPrvTimeVar;
//Must provide analysis start and stop time plus an evaluation step size
dpResult = dpTimeVarying.Exec(startTime, stopTime, stepSize);
break;
default:
break;
}
Array dataValues = null;
IAgDrDataSetCollection datasets = dpResult.DataSets;
if (datasets.Count > 0)
{
IAgDrDataSet thisDataset = datasets.GetDataSetByName(ElementName);
dataValues = thisDataset.GetValues();
}
return(dataValues);
}
public static PropagationResults PropagateAstrogatorSatellite(AgStkObjectRoot root, AgUiApplication app, InitialState state, TLE tle, Data satData, Uncertainty uncertainty, int runId, int nRuns, string propName)
{
PropagationResults propResults = new PropagationResults();
propResults.RunNumber = runId.ToString().PadLeft(3, '0');
IAgSatellite sat = root.CurrentScenario.Children.New(AgESTKObjectType.eSatellite, tle.GetSatNumber() + "Astrogator") as IAgSatellite;
//Set the propagator to Astrogator
sat.SetPropagatorType(AgEVePropagatorType.ePropagatorAstrogator);
//get the Driver for the Propagator
IAgVADriverMCS driver = sat.Propagator as IAgVADriverMCS;
//Clear all segments from the MCS
driver.MainSequence.RemoveAll();
//// Target Sequence ////
IAgVAMCSTargetSequence ts = driver.MainSequence.Insert(AgEVASegmentType.eVASegmentTypeTargetSequence, "SetupState", "-") as IAgVAMCSTargetSequence;
ts.Action = AgEVATargetSeqAction.eVATargetSeqActionRunActiveProfiles;
// add the initial state segment in the target sequence
IAgVAMCSInitialState initState = ts.Segments.Insert(AgEVASegmentType.eVASegmentTypeInitialState, "InitialState", "-") as IAgVAMCSInitialState;
initState.OrbitEpoch = ((IAgScenario)root.CurrentScenario).StartTime;
// define elements
initState.SetElementType(AgEVAElementType.eVAElementTypeCartesian);
IAgVAElementCartesian cart = initState.Element as IAgVAElementCartesian;
cart.X = Convert.ToDouble(state.CartesianPosX);
cart.Y = Convert.ToDouble(state.CartesianPosY);
cart.Z = Convert.ToDouble(state.CartesianPosZ);
cart.Vx = Convert.ToDouble(state.CartesianVelX);
cart.Vy = Convert.ToDouble(state.CartesianVelY);
cart.Vz = Convert.ToDouble(state.CartesianVelZ);
// spacecraft parameters
IAgVASpacecraftParameters spacecraftParameters = (IAgVASpacecraftParameters)initState.SpacecraftParameters;
spacecraftParameters.DryMass = satData.Mass;
spacecraftParameters.Cd = satData.Cd;
spacecraftParameters.DragArea = satData.DragArea;
spacecraftParameters.Cr = satData.Cr;
spacecraftParameters.SolarRadiationPressureArea = satData.SunArea;
spacecraftParameters.RadiationPressureArea = 1e-10;
IAgVAFuelTank fuelTank = (IAgVAFuelTank)initState.FuelTank;
fuelTank.FuelMass = 0;
// enable the control parameter for the state variables
initState.EnableControlParameter(AgEVAControlInitState.eVAControlInitStateCartesianX);
initState.EnableControlParameter(AgEVAControlInitState.eVAControlInitStateCartesianY);
initState.EnableControlParameter(AgEVAControlInitState.eVAControlInitStateCartesianZ);
initState.EnableControlParameter(AgEVAControlInitState.eVAControlInitStateCartesianVx);
initState.EnableControlParameter(AgEVAControlInitState.eVAControlInitStateCartesianVy);
initState.EnableControlParameter(AgEVAControlInitState.eVAControlInitStateCartesianVz);
// add the results
((IAgVAMCSSegment)initState).Results.Add("Relative Motion/InTrack");
IAgVAStateCalcRelMotion intrackRel = ((IAgVAMCSSegment)initState).Results[0] as IAgVAStateCalcRelMotion;
intrackRel.ReferenceSelection = AgEVACalcObjectReference.eVACalcObjectReferenceSpecified;
IAgLinkToObject link_1 = intrackRel.Reference as IAgLinkToObject;
link_1.BindTo("Satellite/" + tle.GetSatNumber().ToString());
((IAgVAMCSSegment)initState).Results.Add("Relative Motion/Radial");
IAgVAStateCalcRelMotion radialRel = ((IAgVAMCSSegment)initState).Results[1] as IAgVAStateCalcRelMotion;
radialRel.ReferenceSelection = AgEVACalcObjectReference.eVACalcObjectReferenceSpecified;
IAgLinkToObject link_2 = radialRel.Reference as IAgLinkToObject;
link_2.BindTo("Satellite/" + tle.GetSatNumber().ToString());
((IAgVAMCSSegment)initState).Results.Add("Relative Motion/CrossTrack");
IAgVAStateCalcRelMotion crosstrackRel = ((IAgVAMCSSegment)initState).Results[2] as IAgVAStateCalcRelMotion;
crosstrackRel.ReferenceSelection = AgEVACalcObjectReference.eVACalcObjectReferenceSpecified;
IAgLinkToObject link_3 = crosstrackRel.Reference as IAgLinkToObject;
link_3.BindTo("Satellite/" + tle.GetSatNumber().ToString());
((IAgVAMCSSegment)initState).Results.Add("Relative Motion/InTrackRate");
IAgVAStateCalcRelMotion intrackrateRel = ((IAgVAMCSSegment)initState).Results[3] as IAgVAStateCalcRelMotion;
intrackrateRel.ReferenceSelection = AgEVACalcObjectReference.eVACalcObjectReferenceSpecified;
IAgLinkToObject link_4 = intrackrateRel.Reference as IAgLinkToObject;
link_4.BindTo("Satellite/" + tle.GetSatNumber().ToString());
((IAgVAMCSSegment)initState).Results.Add("Relative Motion/RadialRate");
IAgVAStateCalcRelMotion radialrateRel = ((IAgVAMCSSegment)initState).Results[4] as IAgVAStateCalcRelMotion;
radialrateRel.ReferenceSelection = AgEVACalcObjectReference.eVACalcObjectReferenceSpecified;
IAgLinkToObject link_5 = radialrateRel.Reference as IAgLinkToObject;
link_5.BindTo("Satellite/" + tle.GetSatNumber().ToString());
((IAgVAMCSSegment)initState).Results.Add("Relative Motion/CrossTrackRate");
IAgVAStateCalcRelMotion crosstrackrateRel = ((IAgVAMCSSegment)initState).Results[5] as IAgVAStateCalcRelMotion;
crosstrackrateRel.ReferenceSelection = AgEVACalcObjectReference.eVACalcObjectReferenceSpecified;
IAgLinkToObject link_6 = crosstrackrateRel.Reference as IAgLinkToObject;
link_6.BindTo("Satellite/" + tle.GetSatNumber().ToString());
/// differential corrector setup ///
IAgVAProfileDifferentialCorrector dc = ts.Profiles["Differential Corrector"] as IAgVAProfileDifferentialCorrector;
// control parameters
IAgVADCControl xControlParam = dc.ControlParameters.GetControlByPaths("InitialState", "InitialState.Cartesian.X");
xControlParam.Enable = true;
xControlParam.MaxStep = 1;
xControlParam.Perturbation = 0.1;
IAgVADCControl yControlParam = dc.ControlParameters.GetControlByPaths("InitialState", "InitialState.Cartesian.Y");
yControlParam.Enable = true;
yControlParam.MaxStep = 1;
yControlParam.Perturbation = 0.1;
IAgVADCControl zControlParam = dc.ControlParameters.GetControlByPaths("InitialState", "InitialState.Cartesian.Z");
zControlParam.Enable = true;
zControlParam.MaxStep = 1;
zControlParam.Perturbation = 0.1;
IAgVADCControl vxControlParam = dc.ControlParameters.GetControlByPaths("InitialState", "InitialState.Cartesian.Vx");
vxControlParam.Enable = true;
vxControlParam.MaxStep = 0.001;
vxControlParam.Perturbation = 1e-04;
IAgVADCControl vyControlParam = dc.ControlParameters.GetControlByPaths("InitialState", "InitialState.Cartesian.Vy");
vyControlParam.Enable = true;
vyControlParam.MaxStep = 0.001;
vyControlParam.Perturbation = 1e-04;
IAgVADCControl vzControlParam = dc.ControlParameters.GetControlByPaths("InitialState", "InitialState.Cartesian.Vz");
vzControlParam.Enable = true;
vzControlParam.MaxStep = 0.001;
vzControlParam.Perturbation = 1e-04;
// results
double[] deviations = uncertainty.GetRandomDeviation();
IAgVADCResult intrackResult = dc.Results.GetResultByPaths("InitialState", "InTrack");
intrackResult.Enable = true;
intrackResult.DesiredValue = deviations[0];
intrackResult.Tolerance = 0.01;
IAgVADCResult radialResult = dc.Results.GetResultByPaths("InitialState", "Radial");
radialResult.Enable = true;
radialResult.DesiredValue = deviations[1];
radialResult.Tolerance = 0.01;
IAgVADCResult crosstrackResult = dc.Results.GetResultByPaths("InitialState", "CrossTrack");
crosstrackResult.Enable = true;
crosstrackResult.DesiredValue = deviations[2];
crosstrackResult.Tolerance = 0.01;
IAgVADCResult intrackRateResult = dc.Results.GetResultByPaths("InitialState", "InTrackRate");
intrackRateResult.Enable = true;
intrackRateResult.DesiredValue = deviations[3] / 1000;
intrackRateResult.Tolerance = 0.001;
IAgVADCResult radialRateResult = dc.Results.GetResultByPaths("InitialState", "RadialRate");
radialRateResult.Enable = true;
radialRateResult.DesiredValue = deviations[4] / 1000;
radialRateResult.Tolerance = 0.001;
IAgVADCResult crosstrackRateResult = dc.Results.GetResultByPaths("InitialState", "CrossTrackRate");
crosstrackRateResult.Enable = true;
crosstrackRateResult.DesiredValue = deviations[5] / 1000;
crosstrackRateResult.Tolerance = 0.001;
/// Propagator ///
IAgVAMCSPropagate propagate = driver.MainSequence.Insert(AgEVASegmentType.eVASegmentTypePropagate, "ToGround", "-") as IAgVAMCSPropagate;
((IAgVAMCSSegment)propagate).Properties.Color = Color.Red;
//propagate.PropagatorName = "CustomProp";
propagate.PropagatorName = propName;
// add an Epoch stopping condition
IAgVAStoppingConditionCollection propStoppingConditions = propagate.StoppingConditions as IAgVAStoppingConditionCollection;
IAgVAStoppingConditionElement epochElement = propStoppingConditions.Add("Epoch");
IAgVAStoppingCondition epoch = (IAgVAStoppingCondition)epochElement.Properties;
epoch.Trip = ((IAgScenario)root.CurrentScenario).StopTime;
// add an Altitude stopping condition
IAgVAStoppingConditionElement altitudeElement = propStoppingConditions.Add("Altitude");
IAgVAStoppingCondition altitude = (IAgVAStoppingCondition)altitudeElement.Properties;
altitude.Trip = 0;
// remove the original stopping condition
propagate.StoppingConditions.Remove("Duration");
// run the MCS
driver.RunMCS();
driver.ClearDWCGraphics();
// get the stop time
IAgDataPrvInterval dp = ((IAgStkObject)sat).DataProviders.GetDataPrvIntervalFromPath("Astrogator MCS Ephemeris Segments") as IAgDataPrvInterval;
IAgDrResult result = dp.Exec(((IAgScenario)root.CurrentScenario).StartTime, ((IAgScenario)root.CurrentScenario).StopTime);
string satStopTime = result.DataSets[3].GetValues().GetValue(1).ToString();
if (satStopTime.Equals((Convert.ToString(((IAgScenario)root.CurrentScenario).StopTime))))
{
// the satellite does not decay (it is propagated until the scenario stop time)
propResults.IsDecayed = false;
}
else
{
propResults.IsDecayed = true;
propResults.ImpactEpoch = satStopTime;
// remove the millisecond part
satStopTime = satStopTime.Split('.')[0];
//ask for LLA data at stop time
IAgDataPrvTimeVar dpInfo = ((IAgStkObject)sat).DataProviders.GetDataPrvInfoFromPath("LLA State//Fixed") as IAgDataPrvTimeVar;
IAgDrResult resInfo = dpInfo.ExecSingle(satStopTime);
string lat = resInfo.DataSets[1].GetValues().GetValue(0).ToString();
string lon = resInfo.DataSets[2].GetValues().GetValue(0).ToString();
string alt = resInfo.DataSets[3].GetValues().GetValue(0).ToString();
propResults.ImpactLat = lat;
propResults.ImpactLon = lon;
propResults.ImpactAlt = alt;
// create a target object
IAgTarget target = root.CurrentScenario.Children.New(AgESTKObjectType.eTarget, "Target" + (runId).ToString().PadLeft(3, '0')) as IAgTarget;
target.Graphics.Color = Color.Red;
target.Graphics.LabelVisible = false;
IAgPosition pos = target.Position;
pos.AssignGeodetic(lat, lon, 0);
// create and display the time event
IAgCrdnProvider provider = root.CurrentScenario.Children["Target" + (runId).ToString().PadLeft(3, '0')].Vgt;
IAgCrdnEventEpoch eventEpoch = provider.Events.Factory.CreateEventEpoch(runId.ToString().PadLeft(3, '0') + "_Impact", "Impact Epoch") as IAgCrdnEventEpoch;
eventEpoch.Epoch = satStopTime;
try { root.ExecuteCommand("Timeline * TimeComponent Add ContentView \"Scenario Availability\" \"Target/Target" + (runId).ToString().PadLeft(3, '0') + " " + runId.ToString().PadLeft(3, '0') + "_Impact Time Instant\""); }
catch (Exception) { }
root.ExecuteCommand("Timeline * Refresh");
// create a unique ephemeris file for each Astrogator run
DateTime now = DateTime.Now;
string satEphemerisPath = Directory.GetCurrentDirectory() + "\\Ephemeris\\Reentry_run_" + (runId).ToString().PadLeft(3, '0') + ".e";
root.ExecuteCommand("ExportDataFile */Satellite/" + tle.GetSatNumber() + "Astrogator Ephemeris \"" + satEphemerisPath + "\" Type STK CoordSys ICRF CentralBody Earth InterpBoundaries Include");
propResults.EphemerisFilePath = satEphemerisPath;
// unload Astrogator satellite
root.CurrentScenario.Children[tle.GetSatNumber() + "Astrogator"].Unload();
if (runId == nRuns)
{
// remove the TLE sat
// root.CurrentScenario.Children[tle.GetSatNumber()].Unload();
}
}
try
{
AGI.Ui.Core.IAgUiWindowsCollection windows = app.Windows;
foreach (dynamic window in app.Windows)
{
string windowCaption = (string)window.Caption;
if (windowCaption.Contains("Setup"))
{
window.Close();
}
}
}
catch (Exception ex)
{
}
return(propResults);
}