Module scenarios 

Pre-built orbital scenarios.

Implements canonical orbital mechanics demonstrations:

• Kepler two-body problem (Earth-Sun)
• N-body solar system
• Hohmann transfer orbits
• Lagrange point dynamics

References

[6] Bate, Mueller, White, “Fundamentals of Astrodynamics,” 1971. [23] Hohmann, “Die Erreichbarkeit der Himmelskörper,” 1925. [24] Szebehely, “Theory of Orbits,” 1967.

Structs

BodyConfig

Single body configuration.

HohmannConfig

Hohmann transfer configuration.

KeplerConfig

Kepler two-body configuration.

LagrangeConfig

Lagrange point configuration.

NBodyConfig

N-body configuration.

Enums

LagrangePoint

Lagrange point selection.

ScenarioType

Scenario type enumeration.