From 73c46fd2f68eb9a52e7bf449c41e6e3988db2f0c Mon Sep 17 00:00:00 2001 From: "copilot-swe-agent[bot]" <198982749+Copilot@users.noreply.github.com> Date: Wed, 3 Dec 2025 20:51:43 +0000 Subject: [PATCH 1/2] Initial plan From 212a5d9908ee0a3bce0fe589fc4e8723037d2844 Mon Sep 17 00:00:00 2001 From: "copilot-swe-agent[bot]" <198982749+Copilot@users.noreply.github.com> Date: Wed, 3 Dec 2025 20:57:03 +0000 Subject: [PATCH 2/2] DOC: Add note about motor file paths in 3-DOF comparison section Co-authored-by: aZira371 <99824864+aZira371@users.noreply.github.com> --- docs/user/three_dof_simulation.rst | 9 +++++++++ 1 file changed, 9 insertions(+) diff --git a/docs/user/three_dof_simulation.rst b/docs/user/three_dof_simulation.rst index dd318af0e..3ac88dca0 100644 --- a/docs/user/three_dof_simulation.rst +++ b/docs/user/three_dof_simulation.rst @@ -464,6 +464,15 @@ with 3-DOF simulations using ``PointMassRocket`` and different weathercocking coefficients. This demonstrates the trade-off between computational speed and accuracy. +.. note:: + + The thrust curve files used in this example (e.g., ``AeroTech_K828FJ.eng``) + are included in the RocketPy repository under the ``data/motors/`` directory. + If you are running this code outside of the repository, you can download the + motor files from `RocketPy's data/motors folder on GitHub + `_ or use + your own thrust curve files. + **Setup the simulations:** .. jupyter-execute::