private void inRange()
{
anomInRange = false;
currentAnomalies = DMAnomalyList.getAnomalyStorage(vessel.mainBody.bodyName);
if (currentAnomalies == null)
{
if (currentAnomaly != null)
{
checkAnomalyDistance(currentAnomaly);
}
}
else
{
for (int i = 0; i < currentAnomalies.AnomalyCount; i++)
{
DMAnomalyObject anom = currentAnomalies.getAnomaly(i);
if (checkAnomalyDistance(anom))
{
break;
}
}
}
if (!anomInRange && camDeployed)
{
animSecondary[foundAnimate].wrapMode = WrapMode.Default;
cam.localRotation = Quaternion.Slerp(cam.localRotation, new Quaternion(0, 0, 0, 1), 1f);
newSecondaryAnimator(camAnimate, -1f, 1f, WrapMode.Default);
camDeployed = false;
}
}
internal void getAnomValues()
{
anomCloseRange = false;
anomScienceInRange = false;
closestAnom = "";
currentAnomalies = DMAnomalyList.getAnomalyStorage(vessel.mainBody.bodyName);
if (currentAnomalies == null)
{
if (currentAnomaly == null)
{
return;
}
checkAnomalyForScience(currentAnomaly);
}
else
{
for (int i = 0; i < currentAnomalies.AnomalyCount; i++)
{
DMAnomalyObject anom = currentAnomalies.getAnomaly(i);
if (checkAnomalyForScience(anom))
{
break;
}
}
}
}
public void Update()
{
if (HighLogic.LoadedSceneIsFlight && primaryModule != null)
{
if (!FlightGlobals.ready || DMScienceScenario.SciScenario == null)
{
return;
}
float deltaTime = 1f;
if (Time.deltaTime != 0)
{
deltaTime = TimeWarp.deltaTime / Time.deltaTime;
}
if (deltaTime > 10)
{
deltaTime = 10;
}
float dTime = Time.time * deltaTime;
if (dTime - lastUpdate > updateInterval || dTime < updateInterval)
{
lastUpdate = Time.time;
if (primaryModule.IsDeployed && runMagnetometer)
{
CelestialBody planetID = vessel.mainBody;
int ID = planetID.flightGlobalsIndex;
//double latDeg; // = (vessel.latitude + 90 + 180) % 180 - 90;
//double lonDeg; // = (vessel.longitude + 180 + 360) % 360 - 180;
double lat;
double lon;
double alt;
double uDay;
double nDay;
int localDay;
long date;
//Paramaters for mag field model
int i = 10;
double[] field = new double[6];
double lonShift;
if (ID == 1 || ID == 2 || ID == 3 || ID == 5 || ID == 6 || ID == 7 || ID == 8 || ID == 9 || ID == 10 || ID == 11 || ID == 12 || ID == 13 || ID == 14)
{
if (ID == 9 || ID == 10 || ID == 11 || ID == 12 || ID == 14)
{
//For now the Joolian moons return values relative to Jool
Vector3 vesselPosition = vessel.transform.position;
alt = FlightGlobals.fetch.bodies[8].GetAltitude(vesselPosition) / 5000;
lat = ((FlightGlobals.fetch.bodies[8].GetLatitude(vesselPosition) + 90 + 180) % 180 - 90) * Mathf.Deg2Rad;
lon = ((FlightGlobals.fetch.bodies[8].GetLongitude(vesselPosition) + 180 + 360) % 360 - 180) * Mathf.Deg2Rad;
planetID = FlightGlobals.fetch.bodies[8];
}
else if (ID == 2 || ID == 3)
{
Vector3 vesselPosition = vessel.transform.position;
alt = FlightGlobals.fetch.bodies[1].GetAltitude(vesselPosition) / 1000;
lat = ((FlightGlobals.fetch.bodies[1].GetLatitude(vesselPosition) + 90 + 180) % 180 - 90) * Mathf.Deg2Rad;
lon = ((FlightGlobals.fetch.bodies[1].GetLongitude(vesselPosition) + 180 + 360) % 360 - 180) * Mathf.Deg2Rad;
planetID = FlightGlobals.fetch.bodies[1];
}
else if (ID == 7)
{
Vector3 vesselPosition = vessel.transform.position;
alt = FlightGlobals.fetch.bodies[6].GetAltitude(vesselPosition) / 1000;
lat = ((FlightGlobals.fetch.bodies[6].GetLatitude(vesselPosition) + 90 + 180) % 180 - 90) * Mathf.Deg2Rad;
lon = ((FlightGlobals.fetch.bodies[6].GetLongitude(vesselPosition) + 180 + 360) % 360 - 180) * Mathf.Deg2Rad;
planetID = FlightGlobals.fetch.bodies[6];
}
else if (ID == 13)
{
Vector3 vesselPosition = vessel.transform.position;
alt = FlightGlobals.fetch.bodies[5].GetAltitude(vesselPosition) / 1000;
lat = ((FlightGlobals.fetch.bodies[5].GetLatitude(vesselPosition) + 90 + 180) % 180 - 90) * Mathf.Deg2Rad;
lon = ((FlightGlobals.fetch.bodies[5].GetLongitude(vesselPosition) + 180 + 360) % 360 - 180) * Mathf.Deg2Rad;
planetID = FlightGlobals.fetch.bodies[5];
}
else
{
lat = ((vessel.latitude + 90 + 180) % 180 - 90) * Mathf.Deg2Rad;
lon = ((vessel.longitude + 180 + 360) % 360 - 180) * Mathf.Deg2Rad;
alt = vessel.altitude / 1000;
if (ID == 8)
{
alt /= 5;
}
}
uDay = Planetarium.GetUniversalTime() / solarDay(planetID);
nDay = uDay % 1;
//Shift our current longitide to account for solar day - lonShift should equal zero when crossing solar noon, bring everything down to -Pi to Pi just to be safe
//For reference, at time zero the sun is directly above -90.158 Deg West on Kerbin, I'm rounding that to -90, or -Pi/2
lonShift = ((lon + longShift(planetID, nDay)) + Math.PI + Math.PI * 2) % (2 * Math.PI) - Math.PI;
//Simulate magnetosphere distortion by solar wind with stretched torus shape, determine our position on the surface of the torus
double radiusx = ((3.5 + (1 + 1 / Math.Cos(lonShift)) * Math.Cos(Math.PI + lonShift)) + (3.5 + (1.3 + 1 / Math.Cos(lonShift)) * Math.Cos(Math.PI + lonShift)) * Math.Cos(lat * 2)) * Math.Cos(lonShift);
double radiusy = (0.75 + 0.9 * Math.Cos(lat * 2)) * Math.Sin(lonShift);
double radiusz = (1 + 0.2 * Math.Cos(lonShift)) * Math.Sin(lat * 2);
double Radius = Math.Sqrt((radiusx * radiusx) + (radiusy * radiusy) + (radiusz * radiusz));
if (Radius == 0)
{
Radius += 0.001;
}
//Scale our altitude by our position on the simulated torus, ignore at altitudes below one planetary radius, ramp up quickly above high scaled altitude up to a max value
if (alt > altScale(planetID))
{
alt *= radScale(planetID) / Radius;
if (alt < altScale(planetID))
{
alt = altScale(planetID);
}
}
if (alt > altScale(planetID) * 2)
{
alt *= Math.Pow((alt / (altScale(planetID) * 2)), 3);
}
if (alt > altMax(planetID))
{
alt = altMax(planetID);
}
}
else if (ID == 0)
{
lat = ((vessel.latitude + 90 + 180) % 180 - 90) * Mathf.Deg2Rad;
lon = ((vessel.longitude + 180 + 360) % 360 - 180) * Mathf.Deg2Rad;
alt = vessel.altitude / 50000;
uDay = Planetarium.GetUniversalTime() / solarDay(planetID);
}
else
{
//For non-magnetic planets use our position relative to the sun to calculate alt, lat, and long
Vector3 vesselPosition = vessel.transform.position;
alt = FlightGlobals.fetch.bodies[0].GetAltitude(vesselPosition) / 50000;
lat = ((FlightGlobals.fetch.bodies[0].GetLatitude(vesselPosition) + 90 + 180) % 180 - 90) * Mathf.Deg2Rad;
lon = ((FlightGlobals.fetch.bodies[0].GetLongitude(vesselPosition) + 180 + 360) % 360 - 180) * Mathf.Deg2Rad;
planetID = FlightGlobals.fetch.bodies[0];
uDay = Planetarium.GetUniversalTime() / solarDay(planetID);
}
localDay = Convert.ToInt32(uDay);
date = 2455197 + (localDay % 500) + ID * 25;
//Send all of our modified parameters to the field model
double[] magComp = getMag(lat, lon, alt, date, i, field);
//Magnetic field components
//double Brad = magComp[0];
//double BPsi = magComp[2];
//double BTheta = magComp[1];
double Bx = magComp[3] * planetScale(planetID);
double By = magComp[4] * planetScale(planetID);
double Bz = magComp[5] * planetScale(planetID);
//Calculate various magenetic field components based on 3-axis field strength
double Bh = Math.Sqrt((Bx * Bx) + (By * By));
//Alter the magnetic field line vector when far away from the planet
if (ID > 0)
{
if (alt > altScale(planetID) * 3)
{
if (ID == 8)
{
if (alt < (altMax(planetID) / 7))
{
Bh /= (alt / (altScale(planetID) * 3));
Bz *= (alt / (altScale(planetID) * 3));
}
else
{
Bh /= ((altMax(planetID) / 7) / (altScale(planetID) * 3));
Bz *= ((altMax(planetID) / 7) / (altScale(planetID) * 3));
}
}
else
{
if (alt < (altMax(planetID) / 2))
{
Bh /= (alt / (altScale(planetID) * 3));
Bz *= (alt / (altScale(planetID) * 3));
}
else
{
Bh /= ((altMax(planetID) / 2) / (altScale(planetID) * 3));
Bz *= ((altMax(planetID) / 2) / (altScale(planetID) * 3));
}
}
}
}
//Anomaly Detection
Cities.Clear();
if (!DMAnomalyList.ScannerUpdating)
{
currentAnomalies = DMAnomalyList.getAnomalyStorage(vessel.mainBody.name);
if (currentAnomalies != null)
{
for (int a = 0; a < currentAnomalies.AnomalyCount; a++)
//foreach (DMAnomalyObject anom in DMScienceScenario.SciScenario.anomalyList.anomObjects())
{
DMAnomalyObject anom = currentAnomalies.getAnomaly(a);
if (anom == null)
{
continue;
}
//foreach (DMAnomalyObject anom in DMScienceScenario.SciScenario.anomalyList.anomObjects())
//{
DMAnomalyList.updateAnomaly(vessel, anom);
if (anom.VDistance < 100000)
{
Cities.Add(anom);
}
}
}
}
else
{
currentAnomalies = DMAnomalyList.getAnomalyStorage(vessel.mainBody.name);
if (currentAnomalies != null)
{
for (int a = 0; a < currentAnomalies.AnomalyCount; a++)
{
//foreach (DMAnomalyObject anom in DMScienceScenario.SciScenario.anomalyList.anomObjects())
//{
DMAnomalyObject anom = currentAnomalies.getAnomaly(a);
if (anom == null)
{
continue;
}
if (anom.VDistance < 100000)
{
Cities.Add(anom);
}
}
}
}
if (Cities.Count > 0)
{
var sortAnom = from entry in Cities orderby entry.VDistance ascending select entry;
var closestAnom = sortAnom.First();
double anomMult = 1d;
double anomMultZ = 1d;
double anomMultH = 1d;
if (closestAnom.VDistance != 0)
{
anomMult = 1 + ((100000 - closestAnom.VDistance) / 10000);
anomMultZ = 1 + (anomMult * ((closestAnom.VDistance - closestAnom.VHorizontal) / closestAnom.VDistance));
anomMultH = 1 + (anomMult * ((closestAnom.VDistance - closestAnom.VHeight) / closestAnom.VDistance));
}
Bz *= anomMultZ;
Bh *= anomMultH;
}
double Bti = Math.Sqrt((Bh * Bh) + (Bz * Bz));
double dip = Math.Atan2(Bz, Bh);
double decD;
//Return 0 declination at magnetic poles
if (Bx != 0.0 || By != 0.0)
{
decD = Math.Atan2(By, Bx);
}
else
{
decD = 0.0;
}
//Convert values for better display
dip *= Mathf.Rad2Deg;
decD *= Mathf.Rad2Deg;
float Btf = (float)Bti;
float incf = (float)dip;
float decf = (float)decD;
float Bzf = (float)Bz;
float Bhf = (float)Bh;
//float BRf = (float)Brad;
//float BPsif = (float)BPsi;
//float BThetaf = (float)BTheta;
//float Bxf = (float)Bx;
//float Byf = (float)By;
//Display in right-click menu
Bt = Btf.ToString("F2") + " nT";
inc = incf.ToString("F2") + "Deg";
dec = decf.ToString("F2") + "Deg";
BhS = Bhf.ToString("F2") + " nT";
BzS = Bzf.ToString("F2") + " nT";
//Br = BRf.ToString("F2") + " nT";
//Bpsi = BPsif.ToString("F2") + " nT";
//Btheta = BThetaf.ToString("F2") + " nT";
//BX = Bxf.ToString("F2") + " nT";
//BY = Byf.ToString("F2") + " nT";
//BZ = Bzf.ToString("F2") + " nT";
Fields["Bt"].guiActive = primaryModule.IsDeployed;
Fields["inc"].guiActive = alt < (altScale(planetID) / 2);
Fields["dec"].guiActive = alt < (altScale(planetID) / 2);
Fields["BhS"].guiActive = alt >= (altScale(planetID) / 2);
Fields["BzS"].guiActive = alt >= (altScale(planetID) / 2);
//Extra variables - used in development
//nDays = nDay.ToString();
//float altf = (float)alt;
//float nDayf = (float)nDay;
//Vector3 sunP = FlightGlobals.fetch.bodies[0].position;
//Vector3 sunD = transform.InverseTransformPoint(sunP) - part.transform.localPosition;
////lons = nDayf.ToString("F5");
//double sunXd = sunD.x;
//double sunZd = sunD.z;
//sunX = sunXd.ToString();
//sunZ = sunZd.ToString();
//lats = altf.ToString("F4");
//nDays = nDayf.ToString("F4");
//radius = Radius.ToString();
//float latf = (float)latDeg;
//lats = (lon * Mathf.Rad2Deg).ToString();
//lons = (lonShift * Mathf.Rad2Deg).ToString();
//float lonf = (float)lonDeg;
//lats = latf.ToString("F3") + " Deg";
//altScaled = alt.ToString();
//lons = lonf.ToString("F3") + " Deg";
//lons = Btf.ToString("F2") + " nT";
//lons = "Shifted long: " + (((lonShift * Mathf.Rad2Deg) + 180 + 360) % 360 - 180).ToString();
//lons = "Scaled Bh: " + Bh.ToString();
//Bznew = "Scaled Bz: " + Bz.ToString();
//Fields["sunX"].guiActive = primaryModule.IsDeployed;
//Fields["sunZ"].guiActive = primaryModule.IsDeployed;
//Fields["lats"].guiActive = primaryModule.IsDeployed;
//Fields["nDays"].guiActive = primaryModule.IsDeployed;
//Fields["lons"].guiActive = primaryModule.IsDeployed;
//Fields["Bhold"].guiActive = primaryModule.IsDeployed;
}
else
{
Fields["Bt"].guiActive = false;
Fields["inc"].guiActive = false;
Fields["dec"].guiActive = false;
Fields["BhS"].guiActive = false;
Fields["BzS"].guiActive = false;
}
}
}
}
public override void OnSave(ConfigNode node)
{
ConfigNode results_node = new ConfigNode("Asteroid_Science");
foreach (DMScienceData data in recoveredDMScience.Values)
{
if (data == null)
{
continue;
}
try
{
ConfigNode scienceResults_node = new ConfigNode("DM_Science");
scienceResults_node.AddValue("title", data.Title);
scienceResults_node.AddValue("bsv", data.BaseValue);
scienceResults_node.AddValue("scv", data.SciVal);
scienceResults_node.AddValue("sci", data.Science);
scienceResults_node.AddValue("cap", data.Cap);
results_node.AddNode(scienceResults_node);
}
catch (Exception e)
{
Debug.LogWarning("[DMagic] Error Saving Asteroid Science Data: " + e);
}
}
ConfigNode anomaly_node = new ConfigNode("Anomaly_Records");
for (int i = 0; i < DMAnomalyList.AnomalyCount; i++)
{
DMAnomalyStorage anomStorage = DMAnomalyList.getAnomalyStorage(i);
if (anomStorage == null)
{
continue;
}
ConfigNode anomalyList = new ConfigNode("DM_Anomaly_List");
anomalyList.AddValue("Body", anomStorage.Body.flightGlobalsIndex);
for (int j = 0; j < anomStorage.AnomalyCount; j++)
{
DMAnomalyObject anom = anomStorage.getAnomaly(j);
if (anom == null)
{
continue;
}
ConfigNode anomaly = new ConfigNode("DM_Anomaly");
anomaly.AddValue("Name", anom.Name);
anomaly.AddValue("Lat", anom.Lat.ToString("N5"));
anomaly.AddValue("Lon", anom.Lon.ToString("N5"));
anomaly.AddValue("Alt", anom.Alt.ToString("N5"));
anomalyList.AddNode(anomaly);
}
anomaly_node.AddNode(anomalyList);
}
node.AddNode(results_node);
node.AddNode(anomaly_node);
}