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MNT: flake8
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MateusStano committed Sep 16, 2024
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Expand Up @@ -1698,7 +1698,6 @@ def u_dot_generalized(
v = Vector([vx, vy, vz]) # CDM velocity vector
e = [e0, e1, e2, e3] # Euler parameters/quaternions
w = Vector([omega1, omega2, omega3]) # Angular velocity vector
omega = [omega1, omega2, omega3]

# Retrieve necessary quantities
## Rocket mass
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