Formatting update

Eci.cpp

@@ -17,8 +17,8 @@ void Eci::ToEci(const Julian& date, const CoordGeodetic &g)
     /*
      * take into account earth flattening
      */
-    const double c = 1.0 /
-        sqrt(1.0 + kF * (kF - 2.0) * pow(sin(g.latitude), 2.0));
+    const double c = 1.0
+        / sqrt(1.0 + kF * (kF - 2.0) * pow(sin(g.latitude), 2.0));
     const double s = pow(1.0 - kF, 2.0) * c;
     const double achcp = (kXKMPER * c + g.altitude) * cos(g.latitude);
 
@@ -54,8 +54,8 @@ CoordGeodetic Eci::ToGeodetic() const
     // 180 >= lon < 180
     const double lon = fmod(theta - date_.ToGreenwichSiderealTime(), kPI);
 
-    const double r = sqrt((position_.x * position_.x) + 
-            (position_.y * position_.y));
+    const double r = sqrt((position_.x * position_.x)
+            + (position_.y * position_.y));
     
     static const double e2 = kF * (2.0 - kF);
 

Observer.cpp

@@ -1,11 +1,10 @@
 #include "Observer.h"
 
-#include "Globals.h"
-
 /*
  * calculate lookangle between the observer and the passed in Eci object
  */
-CoordTopographic Observer::GetLookAngle(const Eci &eci) {
+CoordTopographic Observer::GetLookAngle(const Eci &eci)
+{
 
     /*
      * update the observers Eci to match the time of the Eci passed in
@@ -31,21 +30,23 @@ CoordTopographic Observer::GetLookAngle(const Eci &eci) {
     double sin_theta = sin(theta);
     double cos_theta = cos(theta);
 
-    double top_s = sin_lat * cos_theta * range.x +
-            sin_lat * sin_theta * range.y -
-            cos_lat * range.z;
-    double top_e = -sin_theta * range.x +
-            cos_theta * range.y;
-    double top_z = cos_lat * cos_theta * range.x +
-            cos_lat * sin_theta * range.y +
-            sin_lat * range.z;
+    double top_s = sin_lat * cos_theta * range.x
+        + sin_lat * sin_theta * range.y - cos_lat * range.z;
+    double top_e = -sin_theta * range.x
+        + cos_theta * range.y;
+    double top_z = cos_lat * cos_theta * range.x 
+        + cos_lat * sin_theta * range.y + sin_lat * range.z;
     double az = atan(-top_e / top_s);
 
     if (top_s > 0.0)
+    {
         az += kPI;
+    }
 
     if (az < 0.0)
+    {
         az += 2.0 * kPI;
+    }
 
     double el = asin(top_z / range.w);
     double rate = range.Dot(range_rate) / range.w;