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lla = flat2lla(flatearth_pos, llo, psio, href)
lla = flat2lla(flatearth_pos,
llo, psio, href, ellipsoidModel)
lla = flat2lla(flatearth_pos,
llo, psio, href, flattening, equatorialRadius)
lla = flat2lla(flatearth_pos, llo, psio, href) estimates an array of geodetic coordinates, lla, from an array of flat Earth coordinates, flatearth_pos. This function estimates the lla value with respect to a reference location that llo, psio, and href define.
lla = flat2lla(flatearth_pos, llo, psio, href, ellipsoidModel) estimates the coordinates for a specific ellipsoid planet.
lla = flat2lla(flatearth_pos, llo, psio, href, flattening, equatorialRadius) estimates the coordinates for a custom ellipsoid planet defined by flattening and equatorialRadius.
lla |
m-by-3 array of geodetic coordinates (latitude, longitude, and altitude), in [degrees, degrees, meters]. |
Estimate latitude, longitude, and altitude at a specified coordinate:
lla = flat2lla( [ 4731 4511 120 ], [0 45], 5, -100)
lla =
0.0391 45.0441 -20.0000Estimate latitudes, longitudes, and altitudes at multiple coordinates, specifying the WGS84 ellipsoid model:
lla = flat2lla( [ 4731 4511 120; 0 5074 4498 ], [0 45], 5, -100, 'WGS84' )
lla =
1.0e+003 *
0.0000 0.0450 -0.0200
-0.0000 0.0450 -4.3980Estimate latitudes, longitudes, and altitudes at multiple coordinates, specifying a custom ellipsoid model:
f = 1/196.877360;
Re = 3397000;
lla = flat2lla( [ 4731 4511 120; 0 5074 4498 ], [0 45], 5, -100, f, Re )
lla =
1.0e+003 *
0.0001 0.0451 -0.0200
-0.0000 0.0451 -4.3980The estimation begins by transforming the flat Earth x and y coordinates to North and East coordinates. The transformation has the form of
![]()
where
is the angle in degrees clockwise
between the x-axis and north.
To convert the North and East coordinates to geodetic latitude and longitude, the estimation uses the radius of curvature in the prime vertical (RN) and the radius of curvature in the meridian (RM). (RN) and (RM) are defined by the following relationships:

where (R) is the equatorial radius of the
planet and
is the flattening of the planet.
Small changes in the latitude and longitude are approximated from small changes in the North and East positions by

The output latitude and longitude are the initial latitude and longitude plus the small changes in latitude and longitude.
![]()
The altitude is the negative flat Earth z-axis value minus the reference height (href).
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Etkin, B., Dynamics of Atmospheric Flight. NewYork: John Wiley & Sons, 1972.
Stevens, B. L., and F. L. Lewis, Aircraft Control and Simulation, 2nd ed. New York: John Wiley & Sons, 2003.

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