<reponame>aarondewindt/ae4878_assignments
import numpy as np


# Cartesian frame unit vectors
x_hat = np.array([1, 0, 0])
y_hat = np.array([0, 1, 0])
z_hat = np.array([0, 0, 1])

# Spaceflight constants
mu_earth = 3.98600441e14  # m^3/s^2

# Programming constants
eps64 = np.finfo(np.float64).eps

import numpy as np


# Cartesian frame unit vectors
x_hat = np.array([1, 0, 0])
y_hat = np.array([0, 1, 0])
z_hat = np.array([0, 0, 1])

# Spaceflight constants
mu_earth = 3.98600441e14  # m^3/s^2

# Programming constants
eps64 = np.finfo(np.float64).eps
# Cartesian frame unit vectors # Spaceflight constants # m^3/s^2 # Programming constants