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-rw-r--r--contrib/README4
-rw-r--r--contrib/lla2ecef.c101
2 files changed, 105 insertions, 0 deletions
diff --git a/contrib/README b/contrib/README
index 322af612..4432ac42 100644
--- a/contrib/README
+++ b/contrib/README
@@ -47,3 +47,7 @@ horizon, 13 are tracking, and at least 12 are actually used in a solution.
gpsdlcdd.c is a lcdproc client for gpsd that turns your car computer
into a rudimentary GPS receiver (provided you have at least a 4x40 LCD
screen plugged in and configured to work with lcdproc).
+
+lla2ecef transforms latitude/longitude/altitude (aka north-east-up or local
+tangential plane) coordinates into the earth-centered-earth-fixed frame. If
+invoked as "ecef2lla" it will transform coordinates in the opposite manner.
diff --git a/contrib/lla2ecef.c b/contrib/lla2ecef.c
new file mode 100644
index 00000000..6340ab45
--- /dev/null
+++ b/contrib/lla2ecef.c
@@ -0,0 +1,101 @@
+#include <sys/types.h>
+#include <stdio.h>
+#include <stdlib.h>
+#include <math.h>
+
+extern char *__progname;
+double A = 6378137.0, B = 6356752.3142;
+
+double rad2deg(double r){
+ return (180.0 * r / M_PI);
+}
+
+double deg2rad(double r){
+ return (M_PI * r / 180.0);
+}
+
+void lla2ecef(double *lla, double *ecef){
+ double N;
+
+ lla[0] = deg2rad(lla[0]);
+ lla[1] = deg2rad(lla[1]);
+
+ N = pow(A,2) / sqrt(
+ pow(A,2) * pow(cos(lla[0]),2) +
+ pow(B,2) * pow(sin(lla[0]),2)
+ );
+
+ ecef[0] = (N + lla[2]) * cos(lla[0]) * cos(lla[1]);
+ ecef[1] = (N + lla[2]) * cos(lla[0]) * sin(lla[1]);
+ ecef[2] = (pow(B,2) / pow(A,2) * N + lla[2]) * sin(lla[0]);
+
+ return;
+}
+
+void ecef2lla(double *ecef, double *lla){
+ double E, F, N, P, T;
+
+ E = (pow(A,2) - pow(B,2)) / pow(A,2);
+ F = (pow(A,2) - pow(B,2)) / pow(B,2);
+ P = sqrt(pow(ecef[0], 2) + pow(ecef[1],2));
+
+ T = atan((ecef[2] * A)/(P * B));
+
+ lla[0] = atan(
+ (ecef[2] + F * B * pow(sin(T), 3) ) /
+ (P - E * A * pow(cos(T), 3) )
+ );
+
+ lla[1] = atan( ecef[1] / ecef[0] );
+
+ N = pow(A,2) / sqrt(
+ pow(A,2) * pow(cos(lla[0]),2) +
+ pow(B,2) * pow(sin(lla[0]),2)
+ );
+
+ lla[2] = P / cos(lla[0]) - N;
+ lla[1] = rad2deg(lla[1])-180;
+ lla[0] = rad2deg(lla[0]);
+ return;
+}
+
+int
+main(int argc, char **argv){
+ double ecef[3], lla[3];
+
+ if (4 != argc){
+ printf("usage:\tecef2lla X Y Z\n\tlla2ecef lat lon alt\n");
+ return 1;
+ }
+
+ if (0 == strcmp(__progname, "lla2ecef")){
+ /* Edmonton:
+ lla[0] = 53.52716;
+ lla[1] = -113.53013;
+ lla[2] = 707.0;
+ */
+
+ lla[0] = atof(argv[1]);
+ lla[1] = atof(argv[2]);
+ lla[2] = atof(argv[3]);
+
+ lla2ecef(lla, ecef);
+ printf("%.2lf %.2lf %.2lf\n", ecef[0], ecef[1], ecef[2]);
+ }
+
+ if (0 == strcmp(__progname, "ecef2lla")){
+ /* Edmonton:
+ ecef[0] = -1517110.0;
+ ecef[1] = -3484096.0;
+ ecef[2] = 5106188.0;
+ */
+
+ ecef[0] = atof(argv[1]);
+ ecef[1] = atof(argv[2]);
+ ecef[2] = atof(argv[3]);
+
+ ecef2lla(ecef, lla);
+ printf("%.7lf %.7lf %.2lf\n", lla[0], lla[1], lla[2]);
+ }
+ return 0;
+}