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update orbital_elements struct

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cinnaboot 5 years ago
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f1dc6a1d66
  1. 12
      src/orbits.h

12
src/orbits.h

@ -15,18 +15,28 @@ struct ellipse_parameters
double e; // NOTE: eccentricity
double c; // NOTE: linear eccentricity
double p; // NOTE: semilatus rectum
// FIXME: these should be swapped so f1 is primary focus
glm::vec2 f1; // NOTE: 'vacant' focus
glm::vec2 f2; // NOTE: 'primary' focus
};
struct orbital_elements
{
// NOTE: classical orbital elements
// TODO: would be better to have a higher level composite object so we
// don't have to store this twice
ellipse_parameters ep;
// semimajor axis, a
// eccentricity, e
double iota; // NOTE: (ι) inclination
double omega; // NOTE: (ω) argument of periapsis
double mu; // NOTE: (μ) gravitational parameter
double nu; // NOTE: (ν) true anomaly
// longitude of the ascending node, Ω
// argument of periapsis, ω
// true anomaly at epoch, θ0
#if 1
double mu; // NOTE: (μ) gravitational parameter
double epsilon; // NOTE: (ε) specific orbital energy, MJ/kg
double h; // NOTE: angular momentum

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