Just finished this playlist and I enjoyed immensely. These videos were well detailed but also accesible for those of us who haven't worked with 3Body dynamics before. Thank you professor!
Glad it was helpful! I just posted another in the playlist, and more are planned. Are you working on the 3-body problem? The new video in the series is here czcams.com/video/-QCIFmGYhTQ/video.html and also a recent one introducing industry professionals to satellite dynamics in the Earth-Moon is here czcams.com/video/jmeAML-ekuo/video.html
I greatly appreciate the excellent lectures you have uploaded. I have a question again regarding Ballistic Capture. In the coordinate system where the Moon orbits Earth in a counterclockwise direction, your book's diagram (p.138, (d)) appears to show the Moon rotating clockwise. I assume this is because, when applying a patch in this scenario, the Earth-Moon stable manifold needs to be considered. But does this accurately reflect the actual physical motion? Furthermore, since this manifold rotates with the Moon's orbit, would the EM2 point indicated upon entering the tube be located in a different position at the time of arrival? Lastly, was this diagram created using two PCR3BP models (Earth-Moon-Spacecraft and Sun-Earth-Spacecraft), or was it solved using the BCM four-body problem?
Thank you Professor Ross, these videos are mighty helpful to learn. Could you please tell me if you plan to post next videos of this series any soon? That will be helpful to know.
There are a two more that have already been recorded that I need to edit and post: (1) Trajectories with Prescribed Itineraries, and (2) Halo Orbits - Computing Them and Their Manifolds.
@Dr. Shane Ross In above given MATLAB code for Halo manifolds, in halogesANL(mu,Lpt,Azlp,n) function you have taken k = 2*lambda/(lambda^2 + 1 - c(2)) while as in book and in paper it is k = (lambda^2 + 1 + c(2))/(2*lambda). Can you please plain explain why you have taken it as such.
Just finished this playlist and I enjoyed immensely. These videos were well detailed but also accesible for those of us who haven't worked with 3Body dynamics before. Thank you professor!
Glad it was helpful! I just posted another in the playlist, and more are planned. Are you working on the 3-body problem? The new video in the series is here czcams.com/video/-QCIFmGYhTQ/video.html and also a recent one introducing industry professionals to satellite dynamics in the Earth-Moon is here czcams.com/video/jmeAML-ekuo/video.html
Extremely useful video and details sir... thank you sir
I greatly appreciate the excellent lectures you have uploaded. I have a question again regarding Ballistic Capture. In the coordinate system where the Moon orbits Earth in a counterclockwise direction, your book's diagram (p.138, (d)) appears to show the Moon rotating clockwise. I assume this is because, when applying a patch in this scenario, the Earth-Moon stable manifold needs to be considered. But does this accurately reflect the actual physical motion?
Furthermore, since this manifold rotates with the Moon's orbit, would the EM2 point indicated upon entering the tube be located in a different position at the time of arrival?
Lastly, was this diagram created using two PCR3BP models (Earth-Moon-Spacecraft and Sun-Earth-Spacecraft), or was it solved using the BCM four-body problem?
Thank you Professor Ross, these videos are mighty helpful to learn. Could you please tell me if you plan to post next videos of this series any soon? That will be helpful to know.
There are a two more that have already been recorded that I need to edit and post: (1) Trajectories with Prescribed Itineraries, and (2) Halo Orbits - Computing Them and Their Manifolds.
Yes professor, I am looking forward to them. Thank you for your response.
@Dr. Shane Ross
In above given MATLAB code for Halo manifolds, in halogesANL(mu,Lpt,Azlp,n) function you have taken k = 2*lambda/(lambda^2 + 1 - c(2)) while as in book and in paper it is k = (lambda^2 + 1 + c(2))/(2*lambda). Can you please plain explain why you have taken it as such.