v 0.2.6 Fixed time series length discrepancies, reworked Satellite class

core/dynamics/Satellite.m

@@ -10,7 +10,7 @@ properties
 end
 
 properties(Dependent)
-    vel_orb
+    orbitalVelocity
 end
 
 methods
@@ -20,19 +20,20 @@ methods
 
     end
     
-    function v = get.vel_orb(obj)
-        v = orbitalvelocity(obj.altitude);
+    function v = get.orbitalVelocity(obj)
+        v = sqrt(3.986e14/(obj.altitude+6400)*1e-3);
     end
 
-
     function acc = typicalDragAcc(obj)
         %UNTITLED Summary of this function goes here
         %   Detailed explanation goes here
         rho = Satellite.harrispriester(obj.altitude);
-        acc = 0.5*rho*obj.Cd*obj.area*obj.vel_orb^2 /obj.mass;
+        acc = 0.5*rho*obj.Cd*obj.area*obj.orbitalVelocity^2 /obj.mass;
     end
 end    
 
+
+
 methods (Static)
     function rho = harrispriester(h)
         v = [100 497400.0 497400.0