Motion Near L4, L5 Lagrange Points- Tadpole, Horseshoe Orbit, Trojan Asteroids,Lucy Mission,Topic 12

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  • čas přidán 29. 08. 2024

Komentáře • 6

  • @max-yasgur
    @max-yasgur Před rokem +2

    Great lecture! I hope you’ll discuss more on the spatial problem and halo orbit approximation (Richardson) and higher order generation

    • @ProfessorRoss
      @ProfessorRoss  Před rokem +2

      Thank you and yes, definitely, there will be a lecture on halo orbits, including the Richardson approximation. That is the plan, but there will be a few other lectures first.

  • @krebork
    @krebork Před rokem +1

    So is this channel supposed to prescribed as part of a university course and just happens to be offered on public access?

    • @ProfessorRoss
      @ProfessorRoss  Před rokem +4

      Thanks for watching. This channel is where I post some of my online course content for those who are interested. In fact, this lecture was not part of any official course at any university. I just noticed the content wasn't online anywhere and I'm an expert in the field, so I gave some lectures. Much of my research is in 3-body problem orbital dynamics.

  • @ThompPL1
    @ThompPL1 Před rokem

    33:16 . . . We FINALLY get to see how this mysterious "mu" is actually defined !
    Or I could go back and watch the previous 11 lectures . . . 😉

    • @ProfessorRoss
      @ProfessorRoss  Před rokem

      Sorry you had a difficult time finding the definition of mu. I have endeavored to put it in the description of the lectures, " The mass parameter μ = m2 / (m1 + m2) is the main factor determining the type of motion possible for the spacecraft. It is analogous to the Reynold's number Re in fluid mechanics, as it determines the onset of new types of behavior."