`/*`

*

* ECEF - Earth Centered Earth Fixed

*

* LLA - Lat Lon Alt

*

* ported from matlab code at

*/

// WGS84 ellipsoid constants

private final double a = 6378137; // radius

private final double e = 8.1819190842622e-2; // eccentricity

private final double asq = Math.pow(a,2);

private final double esq = Math.pow(e,2);

private double[] ecef2lla(double[] ecef){

double x = ecef[0];

double y = ecef[1];

double z = ecef[2];

double b = Math.sqrt( asq * (1-esq) );

double bsq = Math.pow(b,2);

double ep = Math.sqrt( (asq – bsq)/bsq);

double p = Math.sqrt( Math.pow(x,2) + Math.pow(y,2) );

double th = Math.atan2(a*z, b*p);

double lon = Math.atan2(y,x);

double lat = Math.atan2( (z + Math.pow(ep,2)*b*Math.pow(Math.sin(th),3) ), (p – esq*a*Math.pow(Math.cos(th),3)) );

double N = a/( Math.sqrt(1-esq*Math.pow(Math.sin(lat),2)) );

double alt = p / Math.cos(lat) – N;

// mod lat to 0-2pi

lon = lon % (2*Math.PI);

// correction for altitude near poles left out.

double[] ret = {lat, lon, alt};

return ret;

}

private double[] lla2ecef(double[] lla){

double lat = lla[0];

double lon = lla[1];

double alt = lla[2];

double N = a / Math.sqrt(1 – esq * Math.pow(Math.sin(lat),2) );

double x = (N+alt) * Math.cos(lat) * Math.cos(lon);

double y = (N+alt) * Math.cos(lat) * Math.sin(lon);

double z = ((1-esq) * N + alt) * Math.sin(lat);

double[] ret = {x, y, z};

return ret;

}

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