vibe coding an orbital mechanics simulation to try out claude code
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# Test Configuration: Spacecraft Maneuvers
# Sun + Earth + LEO Satellite
# Tests basic prograde/retrograde burns in local frame
[[bodies]]
name = "Sun"
mass = 1.989e30
radius = 6.96e8
parent_index = -1
color = { r = 1.0, g = 1.0, b = 0.0 }
orbit = { semi_major_axis = 0.0, eccentricity = 0.0, true_anomaly = 0.0 }
[[bodies]]
name = "Earth"
mass = 5.972e24
radius = 6.371e6
parent_index = 0
color = { r = 0.0, g = 0.5, b = 1.0 }
orbit = { semi_major_axis = 1.496e11, eccentricity = 0.0, true_anomaly = 0.0 }
[[spacecraft]]
name = "LEO_Satellite"
mass = 1000.0
parent_index = 1
orbit = { semi_major_axis = 6.771e6, eccentricity = 0.0, true_anomaly = 0.0 }
# LEO orbit: 400 km altitude (Earth radius 6.371e6 m + 400e3 m)