vibe coding an orbital mechanics simulation to try out claude code
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# Test Configuration: Extreme Eccentricity Orbits
# Tests near-parabolic and hyperbolic orbits
[[bodies]]
name = "Earth"
mass = 5.972e24
radius = 6.371e6
parent_index = -1
color = { r = 0.0, g = 0.5, b = 1.0 }
orbit = {
semi_major_axis = 0.0,
eccentricity = 0.0,
true_anomaly = 0.0
}
[[spacecraft]]
name = "Highly_Elliptical"
mass = 1000.0
parent_index = 0
orbit = {
semi_major_axis = 6.5e8,
eccentricity = 0.99,
true_anomaly = 0.0,
inclination = 0.0,
longitude_of_ascending_node = 0.0,
argument_of_periapsis = 0.0
}
[[spacecraft]]
name = "Near_Parabolic"
mass = 1000.0
parent_index = 0
orbit = {
semi_major_axis = 1.0e9,
eccentricity = 0.95,
true_anomaly = 0.0,
inclination = 0.0,
longitude_of_ascending_node = 0.0,
argument_of_periapsis = 0.0
}
[[spacecraft]]
name = "Slightly_Hyperbolic"
mass = 1000.0
parent_index = 0
orbit = {
semi_major_axis = -1.0e7,
eccentricity = 1.5,
true_anomaly = 0.0,
inclination = 0.0,
longitude_of_ascending_node = 0.0,
argument_of_periapsis = 0.0
}