From e1df0b48f187943d2ec8eb127721ae7f5c0dc905 Mon Sep 17 00:00:00 2001 From: cinnaboot Date: Mon, 5 Jan 2026 13:28:26 -0500 Subject: [PATCH] Add diverse orbit examples to test_simple config MIME-Version: 1.0 Content-Type: text/plain; charset=UTF-8 Content-Transfer-Encoding: 8bit Added bodies to demonstrate different trajectory types: - Parabolic: e=1.0 at 0.5 AU (exactly at escape velocity) - Inclined: circular orbit at 1.2 AU with 30° inclination - Hyperbolic: e=1.5 at 0.5 AU (interstellar visitor trajectory) These showcase the new dynamic orbital rendering capabilities for parabolic, hyperbolic, and inclined orbits. 🤖 Generated with [Claude Code](https://claude.com/claude-code) Co-Authored-By: Claude Sonnet 4.5 --- configs/test_simple.txt | 12 ++++++++++++ 1 file changed, 12 insertions(+) diff --git a/configs/test_simple.txt b/configs/test_simple.txt index 8d7885f..5321f03 100644 --- a/configs/test_simple.txt +++ b/configs/test_simple.txt @@ -26,3 +26,15 @@ Mars 6.39e23 3.3895e6 2.244e11 0 0 0 0.8 0.3 0.1 0 2.244e11 # Comet - eccentric orbit (e=0.7, a=2.5 AU) # At perihelion: 0.75 AU, aphelion: 4.25 AU Comet 1e14 5e3 1.122e11 0 0 0 0.5 0.8 1.0 0.7 3.74e11 + +# Parabolic object - escape trajectory (e=1.0, at perihelion 0.5 AU) +# Exactly at escape velocity +Parabolic 1e13 3e3 7.48e10 0 0 0 1.0 1.0 0.5 1.0 7.48e10 + +# Inclined asteroid - circular orbit at 1.2 AU, 30 deg inclination +# Position: x=1.2AU*cos(0)=1.2AU, y=0, z=1.2AU*sin(30deg)=0.6AU +Inclined 1e12 2e3 1.795e11 0 3.114e10 0 0.8 0.8 0.0 0 1.795e11 + +# Hyperbolic visitor - incoming from interstellar space (e=1.5, a=-1.0 AU) +# At perihelion 0.5 AU with high velocity +Hyperbolic 1e13 3e3 7.48e10 0 0 0 0.3 1.0 0.3 1.5 -1.496e11