Remove plots to fix documentation

sisl · May 28, 2024 · 0e7eef3 · 0e7eef3
1 parent 4b61985
commit 0e7eef3
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Showing 2 changed files with 5 additions and 5 deletions.
diff --git a/docs/make.jl b/docs/make.jl
@@ -19,7 +19,7 @@ makedocs(
         canonical="https://sisl.github.io/SatelliteDynamics.jl",
         edit_link="main",
         assets=String[],
-        prettyurls = false # get(ENV, "CI", nothing) == "true"
+        prettyurls = get(ENV, "CI", nothing) == "true"
     ),
     sitename  = "SatelliteDynamics.jl",
     authors   = "Duncan Eddy",

diff --git a/docs/src/tutorials/orbit_propagation_example.md b/docs/src/tutorials/orbit_propagation_example.md
@@ -73,13 +73,13 @@ t, epc, eci = sim!(orb, epcf)
 And that's it! All it took was 6 lines of code with the SatelliteDynamics 
 module to propagate an orbit. 
 
-We can visualize the orbit in inertial space:
+<!-- We can visualize the orbit in inertial space:
 
 ![](../plots/keplerian_orbit.svg)
 
 Or the evolution of the orbital elements:
 
-![](../plots/keplerian_elements.svg)
+![](../plots/keplerian_elements.svg) -->
 
 ## Full Force Model
 
@@ -112,7 +112,7 @@ orb  = EarthInertialState(epc0, eci0, dt=1.0,
 t, epc, eci = sim!(orb, epcf)
 ```
 
-We can visualize the orbit in inertial space:
+<!-- We can visualize the orbit in inertial space:
 
 ![](../plots/fullforce_orbit.svg)
 
@@ -121,4 +121,4 @@ Or the evolution of the orbital elements:
 ![](../plots/fullforce_elements.svg)
 
 From these plots we can see the effect of the orbit perturbations on each of the
-orbital elements.
+orbital elements. -->