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A Question for Distant Retrograde Orbit in CR3BP

  1. Jun 30, 2018 #1
    In the Sun-Earth system in circular restricted three body problem, how can i define the initial conditions for a distant retrograde orbit? The state vector has to be X=[x0 0 0 0 vy0 0]. How i define the initial position in x-direction and the initial velocity in y-direction.? What values do i give and how do i find these values?

    Thanking you in advance
     
  2. jcsd
  3. Jul 5, 2018 #2
    Thanks for the thread! This is an automated courtesy bump. Sorry you aren't generating responses at the moment. Do you have any further information, come to any new conclusions or is it possible to reword the post? The more details the better.
     
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