Dismiss Notice
Join Physics Forums Today!
The friendliest, high quality science and math community on the planet! Everyone who loves science is here!

Solution of the Geodetic Spherical Equation

  1. Sep 30, 2013 #1
    I have calculated the Keplerian Elements for a particular Position and Velocity Vector for a Satellite around Earth. With a solution of the Geodetic Spherical Equation:
    [tex]u = \frac{1}{R} = \frac{μ}{h^2}(1+ e*Cos(\phi - \tilde\omega))[/tex]
    What does the "R" in this equation represent?

    where ω is the Longitude of the Perigee calculated in the Keplerian Elements.
    [tex]\phi = Acos(\frac{z}{r})[/tex]


    It is strangely similar to this Equation:
    [tex]r = \frac{h^2}{μ}\frac{1}{(1 + e*Cos(TA))}[/tex]
    Where TA is the True Anomaly.
     
    Last edited: Sep 30, 2013
  2. jcsd
Know someone interested in this topic? Share this thread via Reddit, Google+, Twitter, or Facebook

Can you offer guidance or do you also need help?
Draft saved Draft deleted