Still a lot of changes to make

julia/src/inner_loop/inner_loop.jl

@@ -7,8 +7,11 @@ This is it. The outer function call for the inner loop. After this is done,
 there's only the outer loop left to do. And that's pretty easy.
 """
 function inner_loop(launch_date::DateTime,
+                    craft::Sc,
                     phases::Vector{Phase};
-                    min_flyby::Float64=1000.)
+                    min_flyby::Float64=1000.,
+                    mbh_specs=nothing,
+                    verbose=false)
    
   # First we need to do some quick checks that the mission is well formed
   for i in 1:length(phases)
@@ -43,14 +46,24 @@ function inner_loop(launch_date::DateTime,
   end
 
   time = utc2et(Dates.format(launch_date,"yyyy-mm-ddTHH:MM:SS"))
+  thrust_profiles = []
   for phase in phases
     planet1_state = spkssb(ids[phase.from_planet], time, "J2000")
-    println(planet1_state)
     time += phase.time_of_flight
     planet2_state = spkssb(ids[phase.to_planet], time, "J2000")
-    println(planet2_state)
+    # TODO: Come up with improved method of calculating "n"
+    start = planet1_state + [0., 0., 0., phase.v∞_outgoing...]
+    final = planet2_state + [0., 0., 0., phase.v∞_incoming...]
+    if mbh_specs == nothing
+      best = mbh(start, final, craft, μs["Sun"], 0.0, phase.time_of_flight, 10,
+                 verbose=verbose)[1]
+    else
+      best = mbh(start, final, craft, μs["Sun"], 0.0, phase.time_of_flight, 10,
+                 verbose=verbose, num_iters=mbh_specs[1], patience_level=mbh_specs[2])[1]
+    end
+    push!(thrust_profiles, best)
+    craft.mass = prop(tanh.(best.zero), planet1_state, sc, μs["Sun"], prop_time)[2][end]
   end
-
       
-  return phases[1].v∞_incoming[1]
-end
+  return craft.mass, thrust_profiles
+end