public IActionResult Index()
{
DateTime birthday = new DateTime(1991, 6, 5, 8, 26, 00);
Equator equator = Sun.EquatorialCoordinate(birthday);
Ecliptic mooquator = Moon.EclipticalCoordinate(birthday);
Ecliptic merquator = Mercury.EclipticalCoordinate(birthday);
Ecliptic vequator = Venus.EclipticalCoordinate(birthday);
Ecliptic mequator = Mars.EclipticalCoordinate(birthday);
Ecliptic jequator = Jupiter.EclipticalCoordinate(birthday);
Ecliptic sequator = Saturn.EclipticalCoordinate(birthday);
Ecliptic urquator = Uranus.EclipticalCoordinate(birthday);
Ecliptic nequator = Neptune.EclipticalCoordinate(DateTime.Now);
Ecliptic ecliptic = CoordinateSystem.Equatorial2Ecliptic(equator);
Debug.WriteLine(DateTime.Now);
Debug.WriteLine("SUN" + ecliptic.Longitude);
Debug.WriteLine("Moon" + mooquator.Longitude);
Debug.WriteLine("MERC: " + merquator.Longitude);
Debug.WriteLine("VENUS" + vequator.Longitude);
Debug.WriteLine("Mars" + mequator.Longitude);
Debug.WriteLine("Jup: " + jequator.Longitude);
Debug.WriteLine("Saturn: " + sequator.Longitude);
Debug.WriteLine("Urnuas: " + urquator.Longitude);
Debug.WriteLine("Neptune: " + nequator.Longitude);
return(View());
}
private void LoadSolarSystem()
{
_sun = new Sun(DVector2.Zero, DVector2.Zero);
var mercury = new Mercury();
var venus = new Venus();
var earth = new Earth();
var moon = new Moon(earth.Position, earth.Velocity);
var mars = new Mars();
var jupiter = new Jupiter();
var europa = new Europa(jupiter.Position + new DVector2(6.64862e8, 0), jupiter.Velocity + new DVector2(0, -13740));
var saturn = new Saturn();
_massiveBodies = new List <IMassiveBody>
{
_sun, mercury, venus, earth, moon, mars, jupiter, europa, saturn
};
//_spaceCrafts = SpacecraftFactory.BuildFalconHeavy(earth, ProfileDirectory);
//_spaceCrafts = SpacecraftFactory.BuildDragonV2Abort(earth, ProfileDirectory);
_spaceCrafts = SpacecraftFactory.BuildDragonV2Entry(earth, ProfileDirectory);
//_spaceCrafts = SpacecraftFactory.BuildF9(earth, ProfileDirectory);
//_spaceCrafts = SpacecraftFactory.BuildF9Dragon(earth, ProfileDirectory);
// Initialize the spacecraft controllers
foreach (ISpaceCraft spaceCraft in _spaceCrafts)
{
spaceCraft.InitializeController(ProfileDirectory, _eventManager);
}
// Start at nearly -Math.Pi / 2
_strongback = new Strongback(-1.5707947, _spaceCrafts[0].TotalHeight * 0.05, earth);
// Start downrange at ~300km
var asds = new ASDS(-1.62026, 20, earth);
_gravitationalBodies = new List <IGravitationalBody>
{
_sun, mercury, venus, earth
};
foreach (ISpaceCraft spaceCraft in _spaceCrafts)
{
_gravitationalBodies.Add(spaceCraft);
}
_structures = new List <StructureBase>
{
_strongback, //asds
};
_gravitationalBodies.Add(moon);
_gravitationalBodies.Add(mars);
_gravitationalBodies.Add(jupiter);
_gravitationalBodies.Add(europa);
_gravitationalBodies.Add(saturn);
// Target the spacecraft
_targetIndex = _gravitationalBodies.IndexOf(_spaceCrafts.FirstOrDefault());
}
void Update()
{
Sun.Rotate(Vector3.up * Time.deltaTime * 5);
Mercury.RotateAround(Sun.position, new Vector3(0.1f, 1, 0), 60 * Time.deltaTime);
Mercury.Rotate(Vector3.up * 10000 / 58 * Time.deltaTime);
Venus.RotateAround(Sun.position, new Vector3(0, 1, -0.1f), 55 * Time.deltaTime);
Venus.Rotate(Vector3.up * 10000 / 243 * Time.deltaTime);
Earth.RotateAround(Sun.position, Vector3.up, 50 * Time.deltaTime);
Earth.Rotate(Vector3.up * 10000 * Time.deltaTime);
Moon.RotateAround(Earth.position, Vector3.up, 5 * Time.deltaTime);
Moon.Rotate(Vector3.up * 10000 / 27 * Time.deltaTime);
Mars.RotateAround(Sun.position, new Vector3(0.2f, 1, 0), 45 * Time.deltaTime);
Mars.Rotate(Vector3.up * 10000 * Time.deltaTime);
Jupiter.RotateAround(Sun.position, new Vector3(-0.1f, 2, 0), 38 * Time.deltaTime);
Jupiter.Rotate(Vector3.up * 10000 / 0.3f * Time.deltaTime);
Saturn.RotateAround(Sun.position, new Vector3(0, 1, 0.2f), 36 * Time.deltaTime);
Saturn.Rotate(Vector3.up * 10000 / 0.4f * Time.deltaTime);
Uranus.RotateAround(Sun.position, new Vector3(0, 2, 0.1f), 35 * Time.deltaTime);
Uranus.Rotate(Vector3.up * 10000 / 0.6f * Time.deltaTime);
Neptune.RotateAround(Sun.position, new Vector3(-0.1f, 1, -0.1f), 33 * Time.deltaTime);
Neptune.Rotate(Vector3.up * 10000 / 0.7f * Time.deltaTime);
}
public ActionResult DeleteConfirmed(int id)
{
Mercury mercury = db.Mercuries.Find(id);
db.Mercuries.Remove(mercury);
db.SaveChanges();
return(RedirectToAction("Index"));
}
public void OnButtonPressed(VirtualButtonBehaviour vb)
{
if (vb.VirtualButtonName == "previewvb")
{
Sun.SetActive(false);
Mercury.SetActive(false);
Venus.SetActive(false);
Earth.SetActive(false);
Moon.SetActive(false);
Mars.SetActive(false);
Sun1.SetActive(true);
Mercury1.SetActive(true);
Venus1.SetActive(true);
Earth1.SetActive(true);
Moon1.SetActive(true);
Mars1.SetActive(true);
videoplane.SetActive(false);
}
else if (vb.VirtualButtonName == "animationvb")
{
UnityEngine.Debug.Log("animationvb Button pressed");
Sun.SetActive(true);
Mercury.SetActive(true);
Venus.SetActive(true);
Earth.SetActive(true);
Moon.SetActive(true);
Mars.SetActive(true);
Sun1.SetActive(false);
Mercury1.SetActive(false);
Venus1.SetActive(false);
Earth1.SetActive(false);
Moon1.SetActive(false);
Mars1.SetActive(false);
videoplane.SetActive(false);
}
else if (vb.VirtualButtonName == "videovb")
{
UnityEngine.Debug.Log("Traveller Button pressed");
Sun.SetActive(false);
Mercury.SetActive(false);
Venus.SetActive(false);
Earth.SetActive(false);
Moon.SetActive(false);
Mars.SetActive(false);
Sun1.SetActive(false);
Mercury1.SetActive(false);
Venus1.SetActive(false);
Earth1.SetActive(false);
Moon1.SetActive(false);
Mars1.SetActive(false);
videoplane.SetActive(true);
}
else
{
throw new UnityException(vb.VirtualButtonName + "Virtual Button not supported");
}
}
public IActionResult Create([FromBody] Mercury item)
{
if (item == null)
{
return(BadRequest());
}
MercuriesRepo.Add(item);
return(CreatedAtRoute("GetMercuries", new { Controller = "Mercuries", id = item.Mercury_Id }, item));
}
private void image_Tap(object sender, System.Windows.Input.GestureEventArgs e)
{
if (i == 1)
{
Mercury.Begin();
i = 2;
PresentTheAttributes(0);
}
}
public ActionResult Edit([Bind(Include = "Mercury_Id,DateTimeStart,Hg,Unit")] Mercury mercury)
{
if (ModelState.IsValid)
{
db.Entry(mercury).State = EntityState.Modified;
db.SaveChanges();
return(RedirectToAction("Index"));
}
return(View(mercury));
}
public ActionResult Create([Bind(Include = "Mercury_Id,DateTimeStart,Hg,Unit")] Mercury mercury)
{
if (ModelState.IsValid)
{
db.Mercuries.Add(mercury);
db.SaveChanges();
return(RedirectToAction("Index"));
}
return(View(mercury));
}
public async Task Add(Mercury mercuryEntry)
{
try
{
await _context.Mercuries.InsertOneAsync(mercuryEntry);
}
catch (Exception e)
{
throw new Exception("Error during adding Mercury to MongoDB\n" + e.Message);
}
}
static void SeedMercury()
{
MongoClient client = new MongoClient("mongodb://*****:*****@"C:\Users\marti\Desktop\School\AirData\Data\Mercury.xml");
while (xmlReader.Read())
{
// Read node
if ((xmlReader.NodeType == XmlNodeType.Element))
{
if (mercury.DateTimeStart != null && mercury.Hg != 0 && !String.IsNullOrEmpty(mercury.Unit))
{
mercuryCollection.InsertOne(mercury);
mercury = new Mercury();
//Console.WriteLine("new created");
}
if (xmlReader.Name.Equals("DateTimeStart"))
{
mercury.DateTimeStart = DateTime.Parse(xmlReader.ReadElementContentAsString());
//Console.WriteLine("DateTimeStart read");
}
if (xmlReader.Name.Equals("Hg"))
{
mercury.Hg = double.Parse(xmlReader.ReadElementContentAsString());
//Console.WriteLine("Hg read");
}
if (xmlReader.Name.Equals("unit"))
{
mercury.Unit = xmlReader.ReadElementContentAsString();
//Console.WriteLine("unit read");
}
//Console.WriteLine(mercury);
// Insert into DB
Console.WriteLine("So far: " + counter++);
}
}
mercuryCollection.InsertOne(mercury);
Console.WriteLine("Done");
Console.ReadKey();
}
// GET: Mercuries/Delete/5
public ActionResult Delete(int?id)
{
if (id == null)
{
return(new HttpStatusCodeResult(HttpStatusCode.BadRequest));
}
Mercury mercury = db.Mercuries.Find(id);
if (mercury == null)
{
return(HttpNotFound());
}
return(View(mercury));
}
public IActionResult Update(string id, [FromBody] Mercury item)
{
if (item == null)
{
return(BadRequest());
}
var mercuryObj = MercuriesRepo.Find(id);
if (mercuryObj == null)
{
return(NotFound());
}
MercuriesRepo.Update(item);
return(new NoContentResult());
}
private void LoadSolarSystem()
{
_sun = new Sun(DVector2.Zero, DVector2.Zero);
var mercury = new Mercury();
var venus = new Venus();
var earth = new Earth();
_strongback = new Strongback(new DVector2(10, -earth.SurfaceRadius + 38), earth);
var moon = new Moon(earth.Position, earth.Velocity);
var mars = new Mars();
var jupiter = new Jupiter();
var europa = new Europa(jupiter.Position + new DVector2(6.64862e8, 0), jupiter.Velocity + new DVector2(0, -13740));
var saturn = new Saturn();
_massiveBodies = new List <IMassiveBody>
{
_sun, mercury, venus, earth, moon, mars, jupiter, europa, saturn
};
_structures = new List <StructureBase>
{
_strongback
};
_spaceCrafts = SpacecraftFactory.BuildFalconHeavy(earth, ProfileDirectory);
_gravitationalBodies = new List <IGravitationalBody>
{
_sun, mercury, venus, earth
};
foreach (ISpaceCraft spaceCraft in _spaceCrafts)
{
_gravitationalBodies.Add(spaceCraft);
}
_gravitationalBodies.Add(moon);
_gravitationalBodies.Add(mars);
_gravitationalBodies.Add(jupiter);
_gravitationalBodies.Add(europa);
_gravitationalBodies.Add(saturn);
// Target the spacecraft
_targetIndex = _gravitationalBodies.IndexOf(_spaceCrafts.FirstOrDefault());
}
public async Task <UpdateResult> Update(Mercury mercuryEntry)
{
//in reality this is the closest case study I would imagine:
//filter by the time it was taken
var filter = Builders <Mercury> .Filter.Eq(x => x.DateTimeStart, mercuryEntry.DateTimeStart);
//update or correct the measurements
var update = Builders <Mercury> .Update.Set(x => x.Hg, mercuryEntry.Hg);
try
{
return(await _context.Mercuries.UpdateOneAsync(filter, update));
}
catch (Exception e)
{
throw new Exception("Error during updating Mercury using MongoDB\n" + e.Message);
}
}
void Start()
{
Mercury.AddComponent <Planet>().speed = 47.89f;
Venus.AddComponent <Planet>().speed = 35.03f;
Earth.AddComponent <Planet>().speed = 30f;
Mars.AddComponent <Planet>().speed = 24.13f;
Jupiter.AddComponent <Planet>().speed = 13.06f;
Saturn.AddComponent <Planet>().speed = 9.64f;
Uranus.AddComponent <Planet>().speed = 6.81f;
Neptune.AddComponent <Planet>().speed = 5.43f;
Moon.AddComponent <Moon>().speed = 300f;
gs = new GUIStyle
{
fontSize = 35
};
gs.normal.textColor = new Color(1, 0, 0);
gs.fontStyle = FontStyle.Italic;
}
public void Update(Mercury mercuryEntry)
{
//var itemToUpdate = _mercuriesList.FirstOrDefault(m => m.Mercury_Id == mercuryEntry.Mercury_Id);
//if (itemToUpdate != null)
//{
// itemToUpdate.Mercury_Id = mercuryEntry.Mercury_Id;
// itemToUpdate.DateTimeStart = mercuryEntry.DateTimeStart;
// itemToUpdate.Hg = mercuryEntry.Hg;
// itemToUpdate.Unit = mercuryEntry.Unit;
//}
var itemToUpdate = _context.Mercury.FirstOrDefault(m => m.Mercury_Id == mercuryEntry.Mercury_Id);
if (itemToUpdate != null)
{
itemToUpdate.Mercury_Id = mercuryEntry.Mercury_Id;
itemToUpdate.DateTimeStart = mercuryEntry.DateTimeStart;
itemToUpdate.Hg = mercuryEntry.Hg;
itemToUpdate.Unit = mercuryEntry.Unit;
}
_context.SaveChanges();
}
// Start is called before the first frame update
void Start()
{
awa = GetComponentsInChildren <VirtualButtonBehaviour>();
for (int i = 0; i < awa.Length; ++i)
{
awa[i].RegisterOnButtonPressed(OnButtonPressed);
awa[i].RegisterOnButtonReleased(OnButtonReleased);
}
Sun.SetActive(false);
Mercury.SetActive(false);
Venus.SetActive(false);
Earth.SetActive(false);
Moon.SetActive(false);
Mars.SetActive(false);
Sun1.SetActive(false);
Mercury1.SetActive(false);
Venus1.SetActive(false);
Earth1.SetActive(false);
Moon1.SetActive(false);
Mars1.SetActive(false);
videoplane.SetActive(false);
}
private void LoadSolarSystem()
{
_sun = new Sun();
var mercury = new Mercury();
var venus = new Venus();
var earth = new Earth();
var moon = new Moon(earth.Position, earth.Velocity);
var mars = new Mars();
var jupiter = new Jupiter();
var europa = new Europa(jupiter.Position, jupiter.Velocity);
var saturn = new Saturn();
_massiveBodies = new List <IMassiveBody>
{
_sun, mercury, venus, earth, moon, mars, jupiter, europa, saturn
};
ResolveMassiveBodyParents();
_spaceCrafts = new List <ISpaceCraft>();
_structures = new List <StructureBase>();
MissionConfig primaryMission = MissionConfig.Load(ProfilePaths[0]);
_originTime = primaryMission.GetLaunchDate();
OrbitHelper.SimulateToTime(_massiveBodies, _originTime, 300);
// Load missions
for (int i = 0; i < ProfilePaths.Count; i++)
{
MissionConfig missionConfig = MissionConfig.Load(ProfilePaths[i]);
IMassiveBody targetPlanet = LocatePlanet(missionConfig.ParentPlanet);
double launchAngle = targetPlanet.GetSurfaceAngle(_originTime, _sun);
_spaceCrafts.AddRange(SpacecraftFactory.BuildSpaceCraft(targetPlanet, launchAngle, missionConfig, ProfilePaths[i]));
_structures.AddRange(StructureFactory.Load(targetPlanet, launchAngle, ProfilePaths[i]));
}
// Initialize the spacecraft controllers
foreach (ISpaceCraft spaceCraft in _spaceCrafts)
{
spaceCraft.InitializeController(_eventManager);
}
_gravitationalBodies = new List <IGravitationalBody>
{
_sun, mercury, venus, earth, moon, mars, jupiter, europa, saturn
};
foreach (ISpaceCraft spaceCraft in _spaceCrafts)
{
_gravitationalBodies.Add(spaceCraft);
}
// Target the spacecraft
_targetIndex = _gravitationalBodies.IndexOf(_spaceCrafts.FirstOrDefault());
ResolveSpaceCraftParents();
}
public void Add(Mercury mercuryEntry)
{
//_mercuriesList.Add(mercuryEntry);
_context.Mercury.Add(mercuryEntry);
_context.SaveChanges();
}
public void SetMercData()
{
Ecliptic mercquator = Mercury.EclipticalCoordinate(BirthDate);
UserMerc = mercquator.Longitude;
}
private void LoadSolarSystem()
{
_sun = new Sun();
var mercury = new Mercury();
var venus = new Venus();
var earth = new Earth();
var moon = new Moon(earth.Position, earth.Velocity);
var mars = new Mars();
var jupiter = new Jupiter();
var callisto = new Callisto(jupiter.Position, jupiter.Velocity);
var europa = new Europa(jupiter.Position, jupiter.Velocity);
var ganymede = new Ganymede(jupiter.Position, jupiter.Velocity);
var io = new Io(jupiter.Position, jupiter.Velocity);
var saturn = new Saturn();
_massiveBodies = new List <IMassiveBody>
{
_sun, mercury, venus, earth, moon, mars, jupiter, callisto, europa, ganymede, io, saturn
};
ResolveMassiveBodyParents();
_gravitationalBodies = new List <IGravitationalBody>
{
_sun, mercury, venus, earth, moon, mars, jupiter, callisto, europa, ganymede, io, saturn
};
_spaceCraftManager = new SpaceCraftManager(_gravitationalBodies);
_structures = new List <StructureBase>();
MissionConfig primaryMission = MissionConfig.Load(ProfilePaths[0]);
_originTime = primaryMission.GetLaunchDate();
UpdateLoadingPercentage(20);
OrbitHelper.SimulateToTime(_massiveBodies, _originTime, 300, UpdateLoadingPercentage);
UpdateLoadingPercentage(80);
// Load missions
for (int i = 0; i < ProfilePaths.Count; i++)
{
MissionConfig missionConfig = MissionConfig.Load(ProfilePaths[i]);
if (missionConfig.ClockDelay > _clockDelay)
{
_clockDelay = missionConfig.ClockDelay;
}
IMassiveBody targetPlanet = LocatePlanet(missionConfig.ParentPlanet);
// Get the launch angle relative to the sun for the given time at the origin
// and offset each vehicle by a certain amount on the surface
double launchAngle = targetPlanet.GetSurfaceAngle(_originTime, _sun) + i * 0.00002;
_spaceCraftManager.Add(SpacecraftFactory.BuildSpaceCraft(targetPlanet, launchAngle, missionConfig, ProfilePaths[i]));
_structures.AddRange(StructureFactory.Load(targetPlanet, launchAngle, ProfilePaths[i]));
}
_spaceCraftManager.Initialize(_eventManager, _clockDelay);
// Target the spacecraft
_targetIndex = _gravitationalBodies.IndexOf(_spaceCraftManager.First);
_spaceCraftManager.ResolveGravitionalParents(_massiveBodies);
UpdateLoadingPercentage(90);
}
private void LoadSolarSystem()
{
_sun = new Sun();
var mercury = new Mercury();
var venus = new Venus();
var earth = new Earth();
var moon = new Moon(earth.Position, earth.Velocity);
var mars = new Mars();
var jupiter = new Jupiter();
var europa = new Europa(jupiter.Position, jupiter.Velocity);
var saturn = new Saturn();
_massiveBodies = new List <IMassiveBody>
{
_sun, mercury, venus, earth, moon, mars, jupiter, europa, saturn
};
ResolveMassiveBodyParents();
// Simulate the planets out to May 2018 with a 6000 second time step
OrbitHelper.SimulateToTime(_massiveBodies, new DateTime(2018, 5, 1), 300);
_spaceCrafts = new List <ISpaceCraft>();
for (int i = 0; i < ProfileDirectories.Count; i++)
{
string profileDirectory = ProfileDirectories[i];
//List<ISpaceCraft> spaceCraft = SpacecraftFactory.BuildSpaceCraft(mars, profileDirectory, i * 30);
List <ISpaceCraft> spaceCraft = SpacecraftFactory.BuildSpaceCraft(earth, profileDirectory, i * -60);
_spaceCrafts.AddRange(spaceCraft);
}
// Initialize the spacecraft controllers
foreach (ISpaceCraft spaceCraft in _spaceCrafts)
{
spaceCraft.InitializeController(_eventManager);
}
// Start at nearly -Math.Pi / 2
var itsMount = new ITSMount(-1.570795, -69, earth);
var strongback = new Strongback(-1.5708048, -32, earth);
// Start downrange at ~300km
//var asds = new ASDS(-1.8303485, 26, earth);
_gravitationalBodies = new List <IGravitationalBody>
{
_sun, mercury, venus, earth, moon, mars, jupiter, europa, saturn
};
foreach (ISpaceCraft spaceCraft in _spaceCrafts)
{
_gravitationalBodies.Add(spaceCraft);
}
_structures = new List <StructureBase>
{
itsMount,
strongback,
//asds
};
// Target the spacecraft
_targetIndex = _gravitationalBodies.IndexOf(_spaceCrafts.FirstOrDefault());
ResolveSpaceCraftParents();
}
public void Put([FromBody] Mercury value)
{
_mercuriesRepository.Update(value);
}
public void Post([FromBody] Mercury value)
{
_mercuriesRepository.Add(value);
}
public IActionResult Index(double latitude = 39.56, double longitude = 116.23, DateTime time = default, string zone = default)
{
if (time == default)
{
time = DateTime.Now;
}
TimeZoneInfo timeZone;
if (string.IsNullOrEmpty(zone))
{
timeZone = TimeZoneInfo.Local;
}
else
{
timeZone = TimeZoneInfo.FindSystemTimeZoneById(zone);
}
Sun sun = new Sun(latitude, longitude, time, timeZone);
Mercury mercury = new Mercury(latitude, longitude, time, timeZone);
Venus venus = new Venus(latitude, longitude, time, timeZone);
Mars mars = new Mars(latitude, longitude, time, timeZone);
Jupiter jupiter = new Jupiter(latitude, longitude, time, timeZone);
Saturn saturn = new Saturn(latitude, longitude, time, timeZone);
Uranus uranus = new Uranus(latitude, longitude, time, timeZone);
Neptune neptune = new Neptune(latitude, longitude, time, timeZone);
double[] ra = new[] { sun.Equator.RA, mercury.Equator.RA, venus.Equator.RA, mars.Equator.RA,
jupiter.Equator.RA, saturn.Equator.RA, uranus.Equator.RA, neptune.Equator.RA };
double[] dec = new[] { sun.Equator.Dec, mercury.Equator.Dec, venus.Equator.Dec, mars.Equator.Dec,
jupiter.Equator.Dec, saturn.Equator.Dec, uranus.Equator.Dec, neptune.Equator.Dec };
TimeSpan[] rising = new[] { sun.Rising, mercury.Rising, venus.Rising, mars.Rising,
jupiter.Rising, saturn.Rising, uranus.Rising, neptune.Rising };
TimeSpan[] culmination = new[] { sun.Culmination, mercury.Culmination, venus.Culmination, mars.Culmination,
jupiter.Culmination, saturn.Culmination, uranus.Culmination, neptune.Culmination };
TimeSpan[] setting = new[] { sun.Setting, mercury.Setting, venus.Setting, mars.Setting,
jupiter.Setting, saturn.Setting, uranus.Setting, neptune.Setting };
double[] toEarth = new[] { sun.ToEarth, mercury.ToEarth, venus.ToEarth, mars.ToEarth,
jupiter.ToEarth, saturn.ToEarth, uranus.ToEarth, neptune.ToEarth };
double[] toSun = new[] { 0, mercury.ToSun, venus.ToSun, mars.ToSun,
jupiter.ToSun, saturn.ToSun, uranus.ToSun, neptune.ToSun };
double[] ea = new[] { sun.ElevationAngle, mercury.ElevationAngle, venus.ElevationAngle, mars.ElevationAngle,
jupiter.ElevationAngle, saturn.ElevationAngle, uranus.ElevationAngle, neptune.ElevationAngle };
double[] az = new[] { sun.Azimuth, mercury.Azimuth, venus.Azimuth, mars.Azimuth,
jupiter.Azimuth, saturn.Azimuth, uranus.Azimuth, neptune.Azimuth };
ViewData["Latitude"] = latitude;
ViewData["Longitude"] = longitude;
ViewData["Time"] = time;
ViewData["Zone"] = timeZone.Id;
ViewData["RA"] = ra;
ViewData["Dec"] = dec;
ViewData["Rising"] = rising;
ViewData["Culmination"] = culmination;
ViewData["Setting"] = setting;
ViewData["ToEarth"] = toEarth;
ViewData["ToSun"] = toSun;
ViewData["EA"] = ea;
ViewData["Az"] = az;
return(View());
}