a | Orbit | |
Compute(const Vector &dr, const Vector &dv, const double mu) | Orbit | |
Compute(const Body &b, const Body &ref_b) | Orbit | |
e | Orbit | |
GetE() const | Orbit | |
i | Orbit | |
M | Orbit | |
mu | Orbit | |
omega_node | Orbit | |
omega_pericenter | Orbit | |
Orbit() | Orbit | [inline] |
Period() const | Orbit | [inline] |
RelativePosVel(Vector &relative_position, Vector &relative_velocity) const | Orbit |