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/*
Garmin protocol to NMEA 0183 converter
Copyright (C) 2004 Manuel Kasper <mk@neon1.net>.
All rights reserved.
Input:
- D800_Pvt_Data_Type (PID 51)
- satellite data record (PID 114)
Available output sentences:
GPGGA, GPRMC, GPGLL, GPGSA, GPGSV
Known caveats:
- DOP (Dilution of Precision) information not available
(Garmin protocol includes EPE only)
- DGPS information in GPGGA sentence not returned
- speed and course over ground are calculated from the
north/east velocity and may not be accurate
- magnetic variation information not available
- Garmin 16-bit SNR scale unknown
---------------------------------------------------------------------------
Redistribution and use in source and binary forms, with or without
modification, are permitted provided that the following conditions are met:
1. Redistributions of source code must retain the above copyright notice,
this list of conditions and the following disclaimer.
2. Redistributions in binary form must reproduce the above copyright
notice, this list of conditions and the following disclaimer in the
documentation and/or other materials provided with the distribution.
THIS SOFTWARE IS PROVIDED ``AS IS'' AND ANY EXPRESS OR IMPLIED WARRANTIES,
INCLUDING, BUT NOT LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY
AND FITNESS FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
AUTHOR BE LIABLE FOR ANY DIRECT, INDIRECT, INCIDENTAL, SPECIAL, EXEMPLARY,
OR CONSEQUENTIAL DAMAGES (INCLUDING, BUT NOT LIMITED TO, PROCUREMENT OF
SUBSTITUTE GOODS OR SERVICES; LOSS OF USE, DATA, OR PROFITS; OR BUSINESS
INTERRUPTION) HOWEVER CAUSED AND ON ANY THEORY OF LIABILITY, WHETHER IN
CONTRACT, STRICT LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE)
ARISING IN ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
POSSIBILITY OF SUCH DAMAGE.
*/
#include <math.h>
#include <stdio.h>
#include <string.h>
#include <glib.h>
#include "nmea.h"
#include "garmin.h"
#include "nmea-gen.h"
#define NMEA_BUF_SIZE 256
#define NMEA_LATLON_SIZE 16
#define NMEA_UTC_SIZE 16
double g_lastcourse = -1;
void nmea_getutc(D800_Pvt_Data_Type *pvt, char *utctime, char *utcdate) {
int tmp = 0, dtmp=0;
/* UTC time of position fix
Reminder:
pvt->tow = seconds (including fractions) since the start of the week.
pvt->wn_days = days since 31-DEC-1989 for the start of the current week
(neither is adjusted for leap seconds)
pvt->leap_scnds = leap second adjustment required.
*/
/*
The receivers can (and do) return times like 86299.999999 instead
of 86300.0 Rounding is required to get the correct time.
Just capture wn_days for now.
*/
tmp = rint(pvt->tow);
dtmp = pvt->wn_days;
/*
If the result is 604800, it's really the first sample
of the new week, so zero out tmp and increment dtmp
by a week ( 7 days ).
*/
if (tmp >= 604800)
{
dtmp += 7;
tmp = 0;
}
/*
At this point we have tmp = seconds since the start
of the week, and dtmp = the first day of the week.
We now need to correct for leap seconds. This may actually
result in reversing the previous adjustment but the code
required to combine the two operations wouldn't be clear.
*/
tmp -= pvt->leap_scnds;
if (tmp < 0)
{
tmp+= 604800;
dtmp -= 7;
}
/*
Now we have tmp = seconds since the start if the week,
and dtmp = the first day of the week, all corrected for
rounding and leap seconds.
We now convert dtmp to today's day number and tmp to
seconds since midnignt.
*/
dtmp += (tmp / 86400);
tmp %= 86400;
if (utctime) {
int h, m, s;
h = tmp / 3600;
m = (tmp - h*3600) / 60;
s = (tmp - h*3600 - m*60);
sprintf(utctime, "%02d%02d%02d", h, m, s);
}
if (utcdate) {
/* Garmin format: number of days since December 31, 1989 */
unsigned long jd = dtmp + 2447892;
unsigned long w, x, a, b, c, d, e, f;
unsigned long day, month, year;
w = (unsigned long)((jd - 1867216.25)/36524.25);
x = w/4;
a = jd + 1 + w - x;
b = a + 1524;
c = (unsigned long)((b - 122.1)/365.25);
d = (unsigned long)(365.25 * c);
e = (unsigned long)((b-d)/30.6001);
f = (unsigned long)(30.6001 * e);
day = b - d - f;
month = e - 1;
if (month > 12)
month -= 12;
year = c - 4716;
if (month == 1 || month == 2)
year++;
year -= 2000;
sprintf(utcdate, "%02d%02d%02d", day, month, year);
}
}
void nmea_fmtlat(double lat, char *latstr) {
double latdeg, tmp;
latdeg = rad2deg(fabs(lat));
tmp = floor(latdeg);
sprintf(latstr, "%02d%07.4f,%c", (int)tmp, (latdeg - tmp) * 60,
(lat >= 0) ? 'N' : 'S');
}
void nmea_fmtlon(double lon, char *lonstr) {
double londeg, tmp;
londeg = rad2deg(fabs(lon));
tmp = floor(londeg);
sprintf(lonstr, "%03d%07.4f,%c", (int)tmp, (londeg - tmp) * 60,
(lon >= 0) ? 'E' : 'W');
}
/*
nmea_gpgga()
NMEA Global Positioning System Fix Data (GGA)
sat may be NULL (= 0 satellites in view)
Caveats:
- Horizontal dilution of precision (DOP) not available
- DGPS information not available
*/
int nmea_gpgga(D800_Pvt_Data_Type *pvt, cpo_sat_data *sat, char *nmeastc) {
char buf[NMEA_BUF_SIZE];
char slat[NMEA_LATLON_SIZE], slon[NMEA_LATLON_SIZE];
char utc[NMEA_UTC_SIZE];
unsigned char cksum;
int fix, nsat, i;
nmea_getutc(pvt, utc, NULL);
/* latitude */
nmea_fmtlat(pvt->lat, slat);
/* longitude */
nmea_fmtlon(pvt->lon, slon);
/* GPS quality indication */
if (pvt->fix == 0 || pvt->fix == 1)
fix = 0;
else if (pvt->fix == 2 || pvt->fix == 3)
fix = 1;
else if (pvt->fix == 4 || pvt->fix == 5)
fix = 2;
else {
fix = 0;
fprintf(stderr, "WARNING: unknown fix type %d\n", pvt->fix);
}
/* number of satellites in view */
nsat = 0;
if (sat != NULL) {
for (i = 0; i < SAT_MAX_COUNT; i++) {
if (((sat[i].status & SAT_STATUS_MASK) == SAT_STATUS_GOOD) && (sat[i].svid <= MAX_SAT_SVID))
nsat++;
}
}
sprintf(buf, "GPGGA,%s,%s,%s,%d,%02d,,%.1f,M,%.1f,M,,", utc, slat, slon, fix, nsat,
pvt->msl_hght + pvt->alt, -pvt->msl_hght);
cksum = nmea_cksum(buf);
sprintf(nmeastc, "$%s*%02X\r\n", buf, cksum);
return 0;
}
/*
nmea_gprmc()
NMEA Recommended Minimum Specific GPS/TRANSIT Data (RMC)
Caveats:
- Speed and course over ground are calculated from
the north/east velocity and may not be accurate
- Magnetic variation not available
*/
int nmea_gprmc(D800_Pvt_Data_Type *pvt, char *nmeastc) {
char buf[NMEA_BUF_SIZE];
char slat[NMEA_LATLON_SIZE], slon[NMEA_LATLON_SIZE];
char utctime[NMEA_UTC_SIZE], utcdate[NMEA_UTC_SIZE];
double speed, course;
unsigned char cksum;
nmea_getutc(pvt, utctime, utcdate);
/* latitude */
nmea_fmtlat(pvt->lat, slat);
/* longitude */
nmea_fmtlon(pvt->lon, slon);
/* speed over ground */
speed = sqrt(pvt->east*pvt->east + pvt->north*pvt->north) * 3.6 / KNOTS_TO_KMH;
/* course */
if (speed < 1.0) {
if (g_lastcourse >= 0)
course = g_lastcourse;
else
course = 0; /* too low to determine course */
} else {
course = atan2(pvt->east, pvt->north);
if (course < 0)
course += 2*G_PI;
course = rad2deg(course);
g_lastcourse = course; /* remember for later */
}
sprintf(buf, "GPRMC,%s,%c,%s,%s,%05.1f,%05.1f,%s,,", utctime,
(pvt->fix >= 2 && pvt->fix <= 5) ? 'A' : 'V',
slat, slon, speed, course, utcdate);
cksum = nmea_cksum(buf);
sprintf(nmeastc, "$%s*%02X\r\n", buf, cksum);
return 0;
}
/*
nmea_gpgll()
NMEA Geographic Position (GLL)
*/
int nmea_gpgll(D800_Pvt_Data_Type *pvt, char *nmeastc) {
char buf[NMEA_BUF_SIZE];
char slat[NMEA_LATLON_SIZE], slon[NMEA_LATLON_SIZE];
char utctime[NMEA_UTC_SIZE];
unsigned char cksum;
nmea_getutc(pvt, utctime, NULL);
/* latitude */
nmea_fmtlat(pvt->lat, slat);
/* longitude */
nmea_fmtlon(pvt->lon, slon);
sprintf(buf, "GPGLL,%s,%s,%s,%c", slat, slon, utctime,
(pvt->fix >= 2 && pvt->fix <= 5) ? 'A' : 'V');
cksum = nmea_cksum(buf);
sprintf(nmeastc, "$%s*%02X\r\n", buf, cksum);
return 0;
}
/*
nmea_gpgsa()
NMEA GPS DOP and Active Satellites (GSA)
sat may be NULL (= 0 satellites)
Caveats:
- DOP information not available
*/
int nmea_gpgsa(D800_Pvt_Data_Type *pvt, cpo_sat_data *sat, char *nmeastc) {
char buf[NMEA_BUF_SIZE];
int fix, i, nsat = 0;
unsigned char cksum;
if (pvt->fix == 0 || pvt->fix == 1)
fix = 1;
else if (pvt->fix == 2 || pvt->fix == 4)
fix = 2;
else if (pvt->fix == 3 || pvt->fix == 5)
fix = 3;
else {
fix = 1;
fprintf(stderr, "WARNING: unknown fix type %d\n", pvt->fix);
}
sprintf(buf, "GPGSA,A,%d", fix);
if (sat != NULL) {
for (i = 0; i < SAT_MAX_COUNT; i++) {
// if (((sat[i].status & SAT_STATUS_MASK) == SAT_STATUS_GOOD) && (sat[i].svid <= MAX_SAT_SVID) && (sat[i].snr > 0)) {
if (((sat[i].status & SAT_STATUS_MASK) == SAT_STATUS_GOOD) && (sat[i].svid <= MAX_SAT_SVID)) {
#ifdef DEBUG
g_debug ("%s: using sat %2d", __FUNCTION__, sat[i].svid);
#endif
sprintf(buf+strlen(buf), ",%02d", sat[i].svid);
nsat++;
}
else
{
#ifdef DEBUG
g_debug ("%s: not using sat %2d", __FUNCTION__, sat[i].svid);
#endif
}
}
/* pad out the rest of the sentence with commas if needed */
if (nsat < SAT_MAX_COUNT)
for (i = 0; i < (SAT_MAX_COUNT - nsat); i++)
strcat(buf, ",");
} else {
strcat(buf, ",,,,,,,,,,,,");
}
sprintf(buf+strlen(buf), ",,,"); // this should be DOP info
cksum = nmea_cksum(buf);
sprintf(nmeastc, "$%s*%02X\r\n", buf, cksum);
return 0;
}
/*
nmea_gpgsv()
NMEA GPS Satellites in View (GSV)
sat may be NULL (= 0 satellites in view)
Caveats:
- Garmin SNR conversion factor not known
*/
int nmea_gpgsv(cpo_sat_data *sat, char *nmeastc) {
char buf[256];
unsigned char cksum;
int nsat, i, nout, msgi;
if (sat == NULL) {
sprintf(buf, "GPGSV,1,1,00");
cksum = nmea_cksum(buf);
sprintf(nmeastc, "$%s*%02X\r\n", buf, cksum);
return 0;
}
/* scan through the sat array and count the good sats */
nsat = 0;
for (i = 0; i < SAT_MAX_COUNT; i++) {
#ifdef DEBUG
g_debug ("%s: sat %3d: status = %02x SNR = %d", __FUNCTION__, sat[i].svid, sat[i].status & SAT_STATUS_MASK, sat[i].snr);
#endif
if (((sat[i].status & SAT_STATUS_MASK) == SAT_STATUS_GOOD) && (sat[i].svid <= MAX_SAT_SVID)) {
// this should not be needed since a sat with bad SNR will not have good status
// if (sat[i].snr == SAT_SNR_BAD) {
// g_debug ("%s: Sat %02d: bogus SNR = %d", __FUNCTION__, sat[i].svid, sat[i].snr);
// sat[i].snr = 0;
// }
nsat++;
}
}
#ifdef DEBUG
g_debug ("%s: nsat = %d", __FUNCTION__, nsat);
#endif
if (nsat == 0) {
/* build a 'null' GPGSV string */
sprintf(buf, "GPGSV,1,1,00");
cksum = nmea_cksum(buf);
sprintf(nmeastc, "$%s*%02X\r\n", buf, cksum);
} else {
/* scan the array again and build the GPGSV string(s) of active sats */
nout = 0;
msgi = 1;
nmeastc[0] = 0;
sprintf(buf, "GPGSV,%d,%d,%02d", (nsat-1)/4+1, msgi, nsat);
for (i = 0; i < SAT_MAX_COUNT; i++) {
if (((sat[i].status & SAT_STATUS_MASK) == SAT_STATUS_GOOD) && (sat[i].svid <= MAX_SAT_SVID)) {
int snr;
// not needed - see above if (sat[i].snr == 0)
// snr = 0;
// else
snr = sat[i].snr/100; /* empirically, this seems to be the correct factor */
sprintf(buf+strlen(buf), ",%02d,%02d,%03d,%02d",
sat[i].svid, sat[i].elev, sat[i].azmth, snr);
nout++;
/* if we have accumulated a group of 4 sats, write out the string */
if (nout == 4) {
cksum = nmea_cksum(buf);
sprintf(nmeastc+strlen(nmeastc), "$%s*%02X\r\n", buf, cksum);
msgi++;
nout = 0;
sprintf(buf, "GPGSV,%d,%d,%02d", (nsat-1)/4+1, msgi, nsat);
}
}
}
if (nout != 0) {
cksum = nmea_cksum(buf);
sprintf(nmeastc+strlen(nmeastc), "$%s*%02X\r\n", buf, cksum);
}
}
return 0;
}
unsigned char nmea_cksum(char *str) {
int i;
unsigned char cksum = 0;
for (i = 0; str[i]; i++) {
cksum ^= (unsigned char)str[i];
}
return cksum;
}
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