Got plotting working

julia/test/laguerre-conway.jl

@@ -11,7 +11,7 @@
         i += 1
       end
       @test i ≈ T
-      @test orbit ≈ start
+      @test norm(orbit - start) < 1e-2
     end
     for _ in 1:5
       i = 0.
@@ -20,7 +20,7 @@
         i -= 1
       end
       @test i ≈ -T
-      @test orbit ≈ start
+      @test norm(orbit - start) < 1e-2
     end
   end
 

julia/test/plotting.jl

@@ -0,0 +1,18 @@
+@testset "Plotting" begin
+
+  # First some setup
+  sc = Sc("test")
+  T = rand(3600*1.5:0.01:3600*4)
+  start = oe_to_xyz([ (μs["Earth"]*(T/(2π))^2)^(1/3),
+                       0.3,
+                       π/4,
+                       0.,
+                       0.,
+                       1. ], μs["Earth"])
+  ΔVs = [ [1., 1., 1.]/20 for _ in 1:40 ]
+  path = prop(ΔVs, start, sc, μs["Earth"], 0.9T, 40)[1]
+  p = plot_orbits([path])
+  savefig(p,"plot_test.html")
+  @test typeof(p) == PlotlyJS.SyncPlot
+
+end

julia/test/propagator.jl

@@ -14,19 +14,19 @@
   @test laguerre_conway(start, μs["Earth"], stepsize) ≈ propped[1]
 
   # Test that Laguerre-Conway is the default propagator for spacecrafts
-  craft = sc("no_thrust")
+  craft = Sc("no_thrust")
   state, craft = prop_one([0., 0., 0.], start, craft, μs["Earth"], stepsize)
   @test laguerre_conway(start, μs["Earth"], stepsize) ≈ state
   @test craft.mass == 1000.
 
   # Test that mass is reduced properly
-  craft = sc("test")
+  craft = Sc("test")
   start_mass = craft.mass
   state, craft = prop_one([1., 1., 1.]/√(3), start, craft, μs["Earth"], stepsize)
   @test craft.mass == start_mass - craft.mass_flow_rate*stepsize
   
   # Test that a bad ΔV throws an error
-  craft = sc("test")
+  craft = Sc("test")
   start_mass = craft.mass
   @test_throws ErrorException prop_one([1., 1., -1.], start, craft, μs["Earth"], stepsize)
 

julia/test/spacecraft.jl

@@ -1,19 +1,18 @@
 @testset "Spacecraft Construction" begin
 
-  # Test that the standard spacecrafts can be created
-  craft = sc("test")
+  # Test that the standard spacecraft can be created
+  craft = Sc("test")
   @test craft.mass == 1000.
   @test craft.mass_flow_rate == 0.01
   @test craft.max_thrust == 0.1
   @test craft.num_thrusters == 2
   @test craft.duty_cycle == 1.
   
-  craft = sc("no_thrust")
+  craft = Sc("no_thrust")
   @test craft.mass == 1000.
   @test craft.mass_flow_rate == 0.01
   @test craft.max_thrust == 0.
   @test craft.num_thrusters == 0
   @test craft.duty_cycle == 0.
 
-
 end

julia/test/test.jl

@@ -2,19 +2,14 @@ using Test
 using Random
 using LinearAlgebra
 
-# Includes 
-include("../constants.jl")
-include("../conversions.jl")
-include("../spacecraft.jl")
-include("../sft.jl")
-include("../laguerre-conway.jl")
-include("../propagator.jl")
+include("../main.jl")
 
 # Tests
 @testset "All Tests" begin
   include("spacecraft.jl")
   include("laguerre-conway.jl")
   include("propagator.jl")
+  include("plotting.jl")
 end
 
 print()