Example #1
0
        public List <string> GetAvailableDataProviderElements(
            string stkObjectPath, string DataProviderName, string GroupName)
        {
            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;
                    }
                }
            }

            List <string> dataElements = new List <string>();

            for (int i = 0; i < dataProvider.Elements.Count; ++i)
            {
                dataElements.Add(dataProvider.Elements[i].Name);
            }
            return(dataElements);
        }
Example #2
0
        public static double[] GetRICDifferenceAtTCA(string sat1Path, string sat2Path, string epochISOYMD)
        {
            IAgStkObject primary, secondary;

            try
            {
                primary   = StkAssistant.Root.GetObjectFromPath(sat1Path);
                secondary = StkAssistant.Root.GetObjectFromPath(sat2Path);
            }
            catch
            {
                return(null);
            }
            IAgDataProviderInfo dpInfo = primary.DataProviders["RIC Coordinates"];

            IAgDataProvider dataProvider = primary.DataProviders["RIC Coordinates"] as IAgDataProvider;

            dataProvider.PreData = secondary.Path.Replace(StkAssistant.Root.CurrentScenario.Path, "");
            IAgDataPrvTimeVar dpTimeVarying = dataProvider as IAgDataPrvTimeVar;
            Array             elements      = new object[] { "Radial", "In-Track", "Cross-Track" };
            IAgDrResult       dpResult      = dpTimeVarying.ExecSingleElements(epochISOYMD, elements);

            double[] ric = new double[3];
            ric[0] = (double)dpResult.DataSets[0].GetValues().GetValue(0);
            ric[1] = (double)dpResult.DataSets[1].GetValues().GetValue(0);
            ric[2] = (double)dpResult.DataSets[2].GetValues().GetValue(0);

            return(ric);
        }
Example #3
0
        private static IAgDataPrvTimeVar GetClassicalElementsDP(string satPath)
        {
            IAgStkObject primary = Root.GetObjectFromPath(satPath);

            IAgDataProviderGroup classical    = primary.DataProviders["Classical Elements"] as IAgDataProviderGroup;
            IAgDataProvider      dataProvider = classical.Group["ICRF"] as IAgDataProvider;
            //Time varyign data is given as an array of time based values
            IAgDataPrvTimeVar dpTimeVarying = dataProvider as IAgDataPrvTimeVar;

            return(dpTimeVarying);
        }
Example #4
0
        //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);
        }
Example #5
0
        //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");
                }
            }
        }
Example #6
0
        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);
        }
Example #7
0
        public static void MergeEphemeris(IAgStkObject[] objectArray, string outputFilePath)
        {
            Dictionary <double, IAgStkObject> ephems = new Dictionary <double, IAgStkObject>();

            Root.UnitPreferences.SetCurrentUnit("DateFormat", "EpSec");
            foreach (IAgStkObject stkObject in objectArray)
            {
                if (stkObject is IAgSatellite &&
                    (stkObject as IAgSatellite).PropagatorType == AgEVePropagatorType.ePropagatorStkExternal)
                {
                    IAgVePropagatorStkExternal exProp =
                        (stkObject as IAgSatellite).Propagator as IAgVePropagatorStkExternal;
                    if (!ephems.ContainsKey(double.Parse(exProp.StartTime.ToString())))
                    {
                        ephems.Add(double.Parse(exProp.StartTime.ToString()), stkObject);
                    }
                }
            }

            List <KeyValuePair <double, IAgStkObject> > testing = ephems.OrderBy(i => i.Key).ToList();
            List <string> ephemLines = new List <string>();

            for (int i = 0; i < testing.Count(); i++)
            {
                IAgDataProviderGroup dp            = (IAgDataProviderGroup)testing[i].Value.DataProviders["Cartesian Position"];
                IAgDataProvider      dpICRF        = (IAgDataProvider)dp.Group["ICRF"];
                IAgDataPrvTimeVar    dpTimeVarying = (IAgDataPrvTimeVar)dpICRF;

                string stopTime = i < (testing.Count() - 1)
                    ? testing[i + 1].Key.ToString()
                    : ((testing[i].Value as IAgSatellite).Propagator as IAgVePropagatorStkExternal).StopTime.ToString();
                string      startTime = testing[i].Key.ToString();
                IAgDrResult results   = dpTimeVarying.ExecNativeTimes(startTime, stopTime);
                Array       times     = results.DataSets.GetDataSetByName("Time").GetValues();
                Array       xs        = results.DataSets.GetDataSetByName("x").GetValues();
                Array       ys        = results.DataSets.GetDataSetByName("y").GetValues();
                Array       zs        = results.DataSets.GetDataSetByName("z").GetValues();

                dp            = (IAgDataProviderGroup)testing[i].Value.DataProviders["Cartesian Velocity"];
                dpICRF        = (IAgDataProvider)dp.Group["ICRF"];
                dpTimeVarying = (IAgDataPrvTimeVar)dpICRF;

                results = dpTimeVarying.ExecNativeTimes(startTime, stopTime);
                Array xds = results.DataSets.GetDataSetByName("x").GetValues();
                Array yds = results.DataSets.GetDataSetByName("y").GetValues();
                Array zds = results.DataSets.GetDataSetByName("z").GetValues();

                for (int j = 0; j < (times.Length - 2); j++)
                {
                    ephemLines.Add(string.Format("{0}     {1}     {2}     {3}     {4}     {5}     {6}",
                                                 times.GetValue(j), xs.GetValue(j), ys.GetValue(j), zs.GetValue(j), xds.GetValue(j),
                                                 yds.GetValue(j), zds.GetValue(j)));
                }
                //MessageBox.Show("stored values");
            }
            int count = ephemLines.Count;

            ephemLines.Insert(0, "stk.v.10.0");
            ephemLines.Insert(1, "BEGIN Ephemeris");
            ephemLines.Insert(2, "NumberOfEphemerisPoints " + count);
            ephemLines.Insert(3, "InterpolationMethod     Lagrange");
            ephemLines.Insert(4, "InterpolationOrder  5");
            ephemLines.Insert(5,
                              "ScenarioEpoch " +
                              Root.ConversionUtility.ConvertDate(Root.UnitPreferences.GetCurrentUnitAbbrv("DateFormat"), "UTCG",
                                                                 (Root.CurrentScenario as IAgScenario).Epoch.ToString()));
            ephemLines.Insert(6, "CentralBody             Earth");
            ephemLines.Insert(7, "CoordinateSystem        ICRF");
            ephemLines.Insert(8, "DistanceUnit        Meters");
            ephemLines.Insert(9, "EphemerisTimePosVel");

            ephemLines.Add("END Ephemeris");

            File.WriteAllLines(outputFilePath, ephemLines.ToArray());
        }
Example #8
0
        public static RICResults GetRICDifferenceOverTime(string sat1Path, string sat2Path, string epochISOYMD)
        {
            IAgDate tca = StkAssistant.Root.ConversionUtility.NewDate("ISO-YMD", epochISOYMD);

            IAgStkObject primary, secondary;

            try
            {
                primary   = StkAssistant.Root.GetObjectFromPath(sat1Path);
                secondary = StkAssistant.Root.GetObjectFromPath(sat2Path);
            }
            catch
            {
                return(new RICResults());
            }

            double period1 = StkAssistant.GetSatellitePeriod(primary.Path, epochISOYMD);
            double period2 = StkAssistant.GetSatellitePeriod(secondary.Path, epochISOYMD);

            double period = (period1 + period2) / 2;

            IAgDataProviderInfo dpInfo = primary.DataProviders["RIC Coordinates"];

            IAgDataProvider dataProvider = primary.DataProviders["RIC Coordinates"] as IAgDataProvider;

            dataProvider.PreData = secondary.Path.Replace(StkAssistant.Root.CurrentScenario.Path, "");
            IAgDataPrvTimeVar dpTimeVarying = dataProvider as IAgDataPrvTimeVar;
            Array             elements      = new object[] { "Time", "Radial", "In-Track", "Cross-Track", "Range" };
            IAgDrResult       dpResult      = dpTimeVarying.ExecElements(
                tca.Subtract("sec", .5 * period).Format("ISO-YMD"),
                tca.Add("sec", .5 * period).Format("ISO-YMD"),
                10, elements);
            RICResults ricResults = new RICResults();

            foreach (IAgDrDataSet dataset in dpResult.DataSets)
            {
                if (dataset.ElementName.Equals("Time"))
                {
                    List <string> times = new List <string>();
                    foreach (object item in dataset.GetValues())
                    {
                        times.Add(item.ToString());
                    }
                    ricResults.Times = times.ToArray();
                }
                else
                {
                    List <double> values = new List <double>();
                    foreach (object item in dataset.GetValues())
                    {
                        values.Add((double)item);
                    }

                    switch (dataset.ElementName)
                    {
                    case "Radial":
                        ricResults.R = values.ToArray();
                        break;

                    case "In-Track":
                        ricResults.I = values.ToArray();
                        break;

                    case "Cross-Track":
                        ricResults.C = values.ToArray();
                        break;

                    case "Range":
                        ricResults.Range = values.ToArray();
                        break;

                    default:
                        break;
                    }
                }
            }

            return(ricResults);
        }