//pulls data providers for the aircraft in ICRF frame
public static List <Array> GetAttitudeData(IAgStkObject obj, double startTime, double timeStep)
{
List <Array> attitudeData = new List <Array>();
IAgScenario scenario = CommonData.StkRoot.CurrentScenario as IAgScenario;
IAgDrDataSetCollection datasets = null;
if (CommonData.objectClass == "Aircraft")
{
IAgDataProviderGroup attitudeDP1 = obj.DataProviders["Body Axes Orientation:YPR 321"] as IAgDataProviderGroup;
IAgDataPrvTimeVar attitudeDP2 = attitudeDP1.Group["ICRF"] as IAgDataPrvTimeVar;
IAgDrResult result = attitudeDP2.Exec(startTime, scenario.StopTime, timeStep);
datasets = result.DataSets;
}
else if (CommonData.objectClass == "Satellite")
{
IAgDataProviderGroup attitudeDP1 = obj.DataProviders["Attitude YPR"] as IAgDataProviderGroup;
IAgDataPrvTimeVar attitudeDP2 = attitudeDP1.Group["Seq YPR"] as IAgDataPrvTimeVar;
IAgDrResult result = attitudeDP2.Exec(startTime, scenario.StopTime, timeStep);
datasets = result.DataSets;
}
for (int i = 0; i < datasets.Count; i++)
{
attitudeData.Add(datasets[i].GetValues());
}
return(attitudeData);
}
//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 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 void CreateScenarioFromTle(ref AgStkObjectRoot root, double duration, ref InitialState initState, TLE currentTle)
{
root.NewScenario(currentTle.GetSatNumber() + "_Reentry");
DateTime startDate = currentTle.GetTleEpoch();
DateTime stopDate = startDate.AddDays(duration);
IAgScenario scenario = root.CurrentScenario as IAgScenario;
// Set scenario start and stop times
scenario.SetTimePeriod(startDate.ToString("dd MMM yyyy hh:mm:ss.fff"), stopDate.ToString("dd MMM yyyy hh:mm:ss.fff"));
// remove the terrain option
root.ExecuteCommand("Terrain * TerrainServer UseTerrainForAnalysis No");
// create the SGP4 object from the TLE
IAgSatellite decayingSat = (IAgSatellite)root.CurrentScenario.Children.New(AgESTKObjectType.eSatellite, currentTle.GetSatNumber());
decayingSat.SetPropagatorType(AgEVePropagatorType.ePropagatorSGP4);
IAgVePropagatorSGP4 sgp4 = decayingSat.Propagator as IAgVePropagatorSGP4;
sgp4.CommonTasks.AddSegsFromFile(currentTle.GetSatNumber(), currentTle.GetFilePath());
IAgVeGfxAttributesBasic att = decayingSat.Graphics.Attributes as IAgVeGfxAttributesBasic;
att.Color = Color.Yellow;
// Configure time period
sgp4.EphemerisInterval.SetExplicitInterval(scenario.StartTime, scenario.StopTime);
sgp4.Step = 60.0;
// Propagate
sgp4.Propagate();
// change the 3D model
try
{
root.ExecuteCommand("VO */Satellite/" + currentTle.GetSatNumber() + " Model File \"C:\\Program Files\\AGI\\STK 11\\STKData\\VO\\Models\\Misc\\explosion.mdl\"");
}
catch (Exception)
{
}
//// get the initial state from the TLE
initState.Epoch = scenario.StartTime;
IAgDataPrvTimeVar dpPos = ((IAgStkObject)decayingSat).DataProviders.GetDataPrvTimeVarFromPath("Cartesian Position//ICRF");
IAgDrResult resultPos = dpPos.Exec(scenario.StartTime, scenario.StartTime, 60.0);
IAgDrDataSetCollection datasetsPos = resultPos.DataSets;
if (resultPos.DataSets.Count > 0)
{
initState.CartesianPosX = datasetsPos[1].GetValues().GetValue(0).ToString();
initState.CartesianPosY = datasetsPos[2].GetValues().GetValue(0).ToString();
initState.CartesianPosZ = datasetsPos[3].GetValues().GetValue(0).ToString();
}
IAgDataPrvTimeVar dpVel = ((IAgStkObject)decayingSat).DataProviders.GetDataPrvTimeVarFromPath("Cartesian Velocity//ICRF");
IAgDrResult resultVel = dpVel.Exec(scenario.StartTime, scenario.StartTime, 60.0);
IAgDrDataSetCollection datasetsVel = resultVel.DataSets;
if (resultVel.DataSets.Count > 0)
{
initState.CartesianVelX = datasetsVel[1].GetValues().GetValue(0).ToString();
initState.CartesianVelY = datasetsVel[2].GetValues().GetValue(0).ToString();
initState.CartesianVelZ = datasetsVel[3].GetValues().GetValue(0).ToString();
}
// configure the 2D graphics
root.ExecuteCommand("Graphics * BackgroundImage Show Off");
root.ExecuteCommand("MapDetails * LatLon Lon On 15");
root.ExecuteCommand("MapDetails * Map RWDB2_Islands State On Color green");
root.ExecuteCommand("MapDetails * Map RWDB2_International_Borders State On ");
root.ExecuteCommand("MapDetails * Map RWDB2_Lakes State On");
try
{
root.ExecuteCommand("VO * Globe Show On File \"C:\\Program Files\\AGI\\STK 11\\STKData\\VO\\Globes\\Earth\\WhiteOnBlue.glb\"");
}
catch (Exception)
{
}
// configure the 3D graphics
root.ExecuteCommand("VO * GlobeDetails MapDetail Show On Map RWDB2_Coastlines ShowDetail On");
root.ExecuteCommand("VO * GlobeDetails MapDetail Show On Map RWDB2_Islands ShowDetail On DetailColor green");
root.ExecuteCommand("VO * GlobeDetails MapDetail Show On Map RWDB2_Lakes ShowDetail On DetailColor lightblue");
//dynamic uiApp = System.Runtime.InteropServices.Marshal.GetActiveObject("STK11.Application");
//try
//{
// foreach (dynamic window in uiApp.Windows)
// {
// string windowCaption = (string)window.Caption;
// if (windowCaption.Contains("2D"))
// {
// window.DockStyle = 3;
// }
// }
//}
//catch (Exception ex)
//{
// string error = ex.Message;
//}
}
public static TLE CreateScenarioFromSatcat(ref AgStkObjectRoot root, double duration, ref InitialState initState, string satId)
{
root.NewScenario(satId + "_Reentry");
//DateTime startDate = currentTle.GetTleEpoch();
//DateTime stopDate = startDate.AddDays(duration);
IAgScenario scenario = root.CurrentScenario as IAgScenario;
// remove the terrain option
root.ExecuteCommand("Terrain * TerrainServer UseTerrainForAnalysis No");
// import the satellite from the catalog
root.ExecuteCommand("ImportFromDB * Satellite AGIServer Propagate On TimePeriod UseScenarioInterval SSCNumber " + satId + " \"");
// get the satellite start time
IAgStkObject satObj = root.CurrentScenario.Children[0];
IAgSatellite decayingSat = satObj as IAgSatellite;
IAgVePropagatorSGP4 sgp4 = decayingSat.Propagator as IAgVePropagatorSGP4;
//IAgCrdnEventSmartEpoch startEpoch = sgp4.EphemerisInterval.GetStartEpoch();
dynamic startEpoch = sgp4.Segments[0].SwitchTime;
// Set scenario start and stop times
DateTime startDate = STK.GetDateTimeFromStkTimeFormat(Convert.ToString(startEpoch));
DateTime stopDate = startDate.AddDays(duration);
scenario.SetTimePeriod(startDate.ToString("dd MMM yyyy hh:mm:ss.fff"), stopDate.ToString("dd MMM yyyy hh:mm:ss.fff"));
// get the TLE data back from STK
TLE tle = new TLE(startDate, sgp4.Segments[0].SSCNum, Convert.ToString(sgp4.Segments[0].Inclination),
Convert.ToString(sgp4.Segments[0].Eccentricity), Convert.ToString(sgp4.Segments[0].RevNumber),
Convert.ToString(sgp4.Segments[0].MeanMotion));
IAgVeGfxAttributesBasic att = decayingSat.Graphics.Attributes as IAgVeGfxAttributesBasic;
att.Color = Color.Yellow;
// Configure time period
sgp4.EphemerisInterval.SetExplicitInterval(scenario.StartTime, scenario.StopTime);
sgp4.Step = 60.0;
// change the 3D model
try
{
root.ExecuteCommand("VO */Satellite/" + root.CurrentScenario.Children[0].InstanceName + " Model File \"C:\\Program Files\\AGI\\STK 11\\STKData\\VO\\Models\\Misc\\explosion.mdl\"");
}
catch (Exception)
{
}
//// get the initial state from the TLE
initState.Epoch = scenario.StartTime;
IAgDataPrvTimeVar dpPos = ((IAgStkObject)decayingSat).DataProviders.GetDataPrvTimeVarFromPath("Cartesian Position//ICRF");
IAgDrResult resultPos = dpPos.Exec(scenario.StartTime, scenario.StartTime, 60.0);
IAgDrDataSetCollection datasetsPos = resultPos.DataSets;
if (resultPos.DataSets.Count > 0)
{
initState.CartesianPosX = datasetsPos[1].GetValues().GetValue(0).ToString();
initState.CartesianPosY = datasetsPos[2].GetValues().GetValue(0).ToString();
initState.CartesianPosZ = datasetsPos[3].GetValues().GetValue(0).ToString();
}
IAgDataPrvTimeVar dpVel = ((IAgStkObject)decayingSat).DataProviders.GetDataPrvTimeVarFromPath("Cartesian Velocity//ICRF");
IAgDrResult resultVel = dpVel.Exec(scenario.StartTime, scenario.StartTime, 60.0);
IAgDrDataSetCollection datasetsVel = resultVel.DataSets;
if (resultVel.DataSets.Count > 0)
{
initState.CartesianVelX = datasetsVel[1].GetValues().GetValue(0).ToString();
initState.CartesianVelY = datasetsVel[2].GetValues().GetValue(0).ToString();
initState.CartesianVelZ = datasetsVel[3].GetValues().GetValue(0).ToString();
}
// configure the 2D graphics
root.ExecuteCommand("Graphics * BackgroundImage Show Off");
root.ExecuteCommand("MapDetails * LatLon Lon On 15");
root.ExecuteCommand("MapDetails * Map RWDB2_Islands State On Color green");
root.ExecuteCommand("MapDetails * Map RWDB2_International_Borders State On ");
root.ExecuteCommand("MapDetails * Map RWDB2_Lakes State On");
try
{
root.ExecuteCommand("VO * Globe Show On File \"C:\\Program Files\\AGI\\STK 11\\STKData\\VO\\Globes\\Earth\\WhiteOnBlue.glb\"");
}
catch (Exception)
{
}
// configure the 3D graphics
root.ExecuteCommand("VO * GlobeDetails MapDetail Show On Map RWDB2_Coastlines ShowDetail On");
root.ExecuteCommand("VO * GlobeDetails MapDetail Show On Map RWDB2_Islands ShowDetail On DetailColor green");
root.ExecuteCommand("VO * GlobeDetails MapDetail Show On Map RWDB2_Lakes ShowDetail On DetailColor lightblue");
return(tle);
}