Normalize all the line endings

Signed-off-by: Lamont Granquist <[email protected]>
rnlahaye · Aug 26, 2017 · 9bc2fb8 · 9bc2fb8
1 parent 824e322
commit 9bc2fb8
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diff --git a/MechJeb2/CelestialBodyExtensions.cs b/MechJeb2/CelestialBodyExtensions.cs
@@ -1,62 +1,62 @@
-using System;
-using UnityEngine;
-
-namespace MuMech
-{
-    public static class CelestialBodyExtensions
-    {
-        public static double TerrainAltitude(this CelestialBody body, Vector3d worldPosition)
-        {
-            return body.TerrainAltitude(body.GetLatitude(worldPosition), body.GetLongitude(worldPosition));
-        }
-
-        //The KSP drag law is dv/dt = -b * v^2 where b is proportional to the air density and
-        //the ship's drag coefficient. In this equation b has units of inverse length. So 1/b
-        //is a characteristic length: a ship that travels this distance through air will lose a significant
-        //fraction of its initial velocity
-        public static double DragLength(this CelestialBody body, Vector3d pos, double dragCoeff, double mass)
-        {
-            double airDensity = FlightGlobals.getAtmDensity(FlightGlobals.getStaticPressure(pos, body), FlightGlobals.getExternalTemperature(pos, body));
-
-            if (airDensity <= 0) return Double.MaxValue;
-
-            //MechJebCore.print("DragLength " + airDensity.ToString("F5") + " " +  dragCoeff.ToString("F5"));
-
-            return mass / (0.0005 * PhysicsGlobals.DragMultiplier * airDensity * dragCoeff);
-        }
-
-        public static double DragLength(this CelestialBody body, double altitudeASL, double dragCoeff, double mass)
-        {
-            return body.DragLength(body.GetWorldSurfacePosition(0, 0, altitudeASL), dragCoeff, mass);
-        }
-
-        public static double RealMaxAtmosphereAltitude(this CelestialBody body)
-        {
-            return !body.atmosphere ? 0 : body.atmosphereDepth;
-        }
-
-
-        public static double AltitudeForPressure(this CelestialBody body, double pressure)
-        {
-            if (!body.atmosphere)
-                return 0;
-            double upperAlt = body.atmosphereDepth;
-            double lowerAlt = 0;
-            while (upperAlt - lowerAlt > 10)
-            {
-                double testAlt = (upperAlt + lowerAlt) * 0.5;
-                double testPressure = FlightGlobals.getStaticPressure(testAlt, body);
-                if (testPressure < pressure)
-                {
-                    upperAlt = testAlt;
-                }
-                else
-                {
-                    lowerAlt = testAlt;
-                }
-            }
-            return (upperAlt + lowerAlt) * 0.5;
-        }
-
-    }
-}
+using System;
+using UnityEngine;
+
+namespace MuMech
+{
+    public static class CelestialBodyExtensions
+    {
+        public static double TerrainAltitude(this CelestialBody body, Vector3d worldPosition)
+        {
+            return body.TerrainAltitude(body.GetLatitude(worldPosition), body.GetLongitude(worldPosition));
+        }
+
+        //The KSP drag law is dv/dt = -b * v^2 where b is proportional to the air density and
+        //the ship's drag coefficient. In this equation b has units of inverse length. So 1/b
+        //is a characteristic length: a ship that travels this distance through air will lose a significant
+        //fraction of its initial velocity
+        public static double DragLength(this CelestialBody body, Vector3d pos, double dragCoeff, double mass)
+        {
+            double airDensity = FlightGlobals.getAtmDensity(FlightGlobals.getStaticPressure(pos, body), FlightGlobals.getExternalTemperature(pos, body));
+
+            if (airDensity <= 0) return Double.MaxValue;
+
+            //MechJebCore.print("DragLength " + airDensity.ToString("F5") + " " +  dragCoeff.ToString("F5"));
+
+            return mass / (0.0005 * PhysicsGlobals.DragMultiplier * airDensity * dragCoeff);
+        }
+
+        public static double DragLength(this CelestialBody body, double altitudeASL, double dragCoeff, double mass)
+        {
+            return body.DragLength(body.GetWorldSurfacePosition(0, 0, altitudeASL), dragCoeff, mass);
+        }
+
+        public static double RealMaxAtmosphereAltitude(this CelestialBody body)
+        {
+            return !body.atmosphere ? 0 : body.atmosphereDepth;
+        }
+
+
+        public static double AltitudeForPressure(this CelestialBody body, double pressure)
+        {
+            if (!body.atmosphere)
+                return 0;
+            double upperAlt = body.atmosphereDepth;
+            double lowerAlt = 0;
+            while (upperAlt - lowerAlt > 10)
+            {
+                double testAlt = (upperAlt + lowerAlt) * 0.5;
+                double testPressure = FlightGlobals.getStaticPressure(testAlt, body);
+                if (testPressure < pressure)
+                {
+                    upperAlt = testAlt;
+                }
+                else
+                {
+                    lowerAlt = testAlt;
+                }
+            }
+            return (upperAlt + lowerAlt) * 0.5;
+        }
+
+    }
+}