Currently working on refactor, much work to do

julia/test/plotting.jl

@@ -4,21 +4,32 @@
 
   using PlotlyJS
 
-  # First some setup
-  sc = Sc("test")
-  T = rand(3600*2:0.01:3600*4)
-  start = [oe_to_xyz([ (μs["Earth"]*(T/(2π))^2)^(1/3),
-                        0.1,
-                        π/4,
-                        0.,
-                        0.,
-                        1. ], μs["Earth"]); 10_000.]
+  # Plot an earth plot
+  T = rand(2hour : 1 : 4hour)
   revs = 30
   n = revs*100
-  ΔVs = repeat([0.9, 0., 0.]', outer=(n,1))
-  path = prop(ΔVs, start, copy(sc), μs["Earth"], revs*T)[1]
-  p = plot_orbits([path])
-  savefig(p,"../plots/plot_test.html")
+
+  start = gen_orbit(T, 12_000., Earth)
+  thrust = spiral(0.9, n, start, test_sc, revs*T, Earth)
+  path = prop(thrust, start, test_sc, revs*T, Earth)[1]
+
+  p = plot_orbits([path], Earth)
+  savefig(p,"../plots/plot_test_earth.html")
   @test typeof(p) == PlotlyJS.SyncPlot
 
+  # Now change a little bit and plot around the Sun
+  # This also checks that the spacecraft are configured right:
+  #   They really shouldn't run out of fuel in 4 years
+  T = rand(year : hour : 4year)
+  tof = 4year
+  start = gen_orbit(T, 12_000.)
+  thrust = spiral(0.9, n, start, bepi, tof)
+  sun_paths = Vector{Vector{Vector{Float64}}}()
+  push!(sun_paths, prop(zeros(100,3), start, bepi, tof)[1])
+  push!(sun_paths, prop(thrust, start, bepi, tof)[1])
+  p = plot_orbits(sun_paths)
+  savefig(p,"../plots/plot_test_sun.html")
+  @test typeof(p) == PlotlyJS.SyncPlot
+
+
 end