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I am trying to convert an ECEF coordinate to a geodetic coordinate using this procedure, but I don't fully understand the process. It is prefaced by stating the geodetic parameters {a,b,e,e'} are assumed to be known, but does not state what they reference to.

I assume that a and b are the equatorial and polar semi-axes, and that e is just Euler's number. Am I correct in this? And what is e' supposed to be?

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    What software are you using? What have you tried so far?
    – MaryBeth
    Commented Dec 19, 2017 at 18:48
  • @MaryBeth I'm writing the conversion as a function in Java. I've researched a few different methods for converting ECEF to Geodetic (e.g. Zhu referenced by wikipedia), but this one is most easily translatable into Java code. I can't figure out what the known parameters are reference to though.
    – Derek S.
    Commented Dec 19, 2017 at 18:56

4 Answers 4

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You can use this function to perform the conversion of ECEF coordinates to Geodetic coordinates.

The function is implemented in python but can be easily written in java.

Example:

import math

def xyz2llh(x,y,z):
    '''
    Function to convert xyz ECEF to llh
    convert cartesian coordinate into geographic coordinate
    ellipsoid definition: WGS84
      a= 6,378,137m
      f= 1/298.257

    Input
      x: coordinate X meters
      y: coordinate y meters
      z: coordinate z meters
    Output
      lat: latitude rad
      lon: longitude rad
      h: height meters
    '''
    # --- WGS84 constants
    a = 6378137.0
    f = 1.0 / 298.257223563
    # --- derived constants
    b = a - f*a
    e = math.sqrt(math.pow(a,2.0)-math.pow(b,2.0))/a
    clambda = math.atan2(y,x)
    p = math.sqrt(pow(x,2.0)+pow(y,2))
    h_old = 0.0
    # first guess with h=0 meters
    theta = math.atan2(z,p*(1.0-math.pow(e,2.0)))
    cs = math.cos(theta)
    sn = math.sin(theta)
    N = math.pow(a,2.0)/math.sqrt(math.pow(a*cs,2.0)+math.pow(b*sn,2.0))
    h = p/cs - N
    while abs(h-h_old) > 1.0e-6:
        h_old = h
        theta = math.atan2(z,p*(1.0-math.pow(e,2.0)*N/(N+h)))
        cs = math.cos(theta)
        sn = math.sin(theta)
        N = math.pow(a,2.0)/math.sqrt(math.pow(a*cs,2.0)+math.pow(b*sn,2.0))
        h = p/cs - N
    llh = {'lon':clambda, 'lat':theta, 'height': h}
    return llh
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After some more research (from here and here), I believe e and e' refer to first and second eccentricity, while a and b do indeed refer to the equatorial and polar semi-axes. Hopefully somebody can confirm this, as I am not 100% certain.

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    You're correct. e'^2 is defined in the "The application of Ferrari's solution" and e^2 is defined earlier in the "From geodetic to ECEF coordinates" section.
    – mkennedy
    Commented Dec 19, 2017 at 19:55
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a is one of the defining parameters; and b, e, and e' are some of the derived geometric constants of the WGS84 ellipsoid.

e is the first eccentricity. e' is the second eccentricity.

See page 3-2 and table 3.5 in NGA STND 0036_1 0 0_WGS84.pdf

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A better way of doing it can be found at the end of this document: https://hal.archives-ouvertes.fr/hal-01704943v2/document

In this document, it's explained how to do it properly and including a C code so it's easy to copy and paste to see if the solution works.

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