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 <noreply@anthropic.com>
Extend config format to support both circular and eccentric orbits using
eccentricity and semi-major axis parameters. All bodies now use the same
format: e=0 for circular orbits, e>0 for eccentric orbits.
Velocity calculation uses vis-viva equation for all cases. Add example
comet with highly eccentric orbit (e=0.7) to test configuration.
🤖 Generated with [Claude Code](https://claude.com/claude-code)
- Sun + Earth (1 AU) + Mars (1.5 AU)
- Circular orbits in XY plane
- Easy to verify: Earth 365 day period, Mars 687 day period
- Minimal 3-body system for testing orbital mechanics
🤖 Generated with [Claude Code](https://claude.com/claude-code)
Co-Authored-By: Claude Sonnet 4.5 <noreply@anthropic.com>
cinnaboot