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J2 Perturbation Part 2 | Orbital Mechanics with Python 11
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In this video I go over a few extra details about the J2 perturbation. I address a small mistake I made in the previous video, regarding the plotting of the semi-major axis. I believe the error in the previous video is due to the 'lsoda' differential equation solver that I have found has certain issues in certain perturbations, but need to look further into it. I also talk more about the Variation of Parameters method for the J2 perturbation and how it is dependent on inclination. I finish by showing some examples of special inclinations where some keplerian orbital elements are not affected by the J2 perturbation.
Here is the J2 perturbation in the ODE implementation:
# J2 perturbation
z2 = r[ 2 ] ** 2
r2 = norm_r ** 2
tx = r[ 0 ] / norm_r * ( 5 * z2 / r2 - 1 )
ty = r[ 1 ] / norm_r * ( 5 * z2 / r2 - 1 )
tz = r[ 2 ] / norm_r * ( 5 * z2 / r2 - 3 )
Pre-req videos:
Optional videos:
Also I think I fixed the mic issue, sorry about that.
Link to video explaining J2:
Here is the J2 perturbation in the ODE implementation:
# J2 perturbation
z2 = r[ 2 ] ** 2
r2 = norm_r ** 2
tx = r[ 0 ] / norm_r * ( 5 * z2 / r2 - 1 )
ty = r[ 1 ] / norm_r * ( 5 * z2 / r2 - 1 )
tz = r[ 2 ] / norm_r * ( 5 * z2 / r2 - 3 )
Pre-req videos:
Optional videos:
Also I think I fixed the mic issue, sorry about that.
Link to video explaining J2:
J2 Perturbation Part 2 | Orbital Mechanics with Python 11
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