From d819aa9e97fa8561c0555df454022807ba66d6da Mon Sep 17 00:00:00 2001 From: jmpenn Date: Sun, 27 Sep 2020 19:22:55 -0500 Subject: [PATCH] Update README.md --- .../trick_utils/SAIntegrator/examples/Orbit/README.md | 8 ++++---- 1 file changed, 4 insertions(+), 4 deletions(-) diff --git a/trick_source/trick_utils/SAIntegrator/examples/Orbit/README.md b/trick_source/trick_utils/SAIntegrator/examples/Orbit/README.md index 6f87c0a3..6a5fd88e 100644 --- a/trick_source/trick_utils/SAIntegrator/examples/Orbit/README.md +++ b/trick_source/trick_utils/SAIntegrator/examples/Orbit/README.md @@ -3,15 +3,15 @@ This program uses the *SemiImplicitEuler* integrator to simulate the orbit of an Earth satellite. Generate the results as follows: -''' +``` $ make $ ./Orbit > orbit.csv -''' +``` Plot the results as follows: -''' +``` $ python plot_position.py -''' +``` ![Orbit](images/Orbit.png)