//
// Written by Curtis Olson, started November 1999.
//
-// Copyright (C) 1999 Curtis L. Olson - curt@flightgear.org
+// Copyright (C) 1999 Curtis L. Olson - http://www.flightgear.org/~curt
//
// This program is free software; you can redistribute it and/or
// modify it under the terms of the GNU General Public License as
//
// You should have received a copy of the GNU General Public License
// along with this program; if not, write to the Free Software
-// Foundation, Inc., 675 Mass Ave, Cambridge, MA 02139, USA.
+// Foundation, Inc., 51 Franklin Street, Fifth Floor, Boston, MA 02110-1301, USA.
//
// $Id$
+#ifdef HAVE_CONFIG_H
+# include "config.h"
+#endif
+
+#include <cstring>
#include <simgear/debug/logstream.hxx>
#include <simgear/math/sg_geodesy.hxx>
#include <simgear/io/iochannel.hxx>
#include <simgear/timing/sg_time.hxx>
-#include <FDM/flight.hxx>
+#include <FDM/flightProperties.hxx>
#include <Main/fg_props.hxx>
#include <Main/globals.hxx>
#include "nmea.hxx"
-SG_USING_NAMESPACE(std);
-
-
FGNMEA::FGNMEA() {
+ fdm = new FlightProperties();
}
FGNMEA::~FGNMEA() {
+ delete fdm;
}
t->getGmt()->tm_hour, t->getGmt()->tm_min, t->getGmt()->tm_sec );
char gga_lat[20], rmc_lat[20];
- double latd = cur_fdm_state->get_Latitude() * SGD_RADIANS_TO_DEGREES;
+ double latd = fdm->get_Latitude() * SGD_RADIANS_TO_DEGREES;
if ( latd < 0.0 ) {
latd = -latd;
dir = 'S';
}
deg = (int)(latd);
min = (latd - (double)deg) * 60.0;
- sprintf( gga_lat, "%02d%06.3f,%c", abs(deg), min, dir);
+ sprintf( gga_lat, "%02d%07.4f,%c", abs(deg), min, dir);
sprintf( rmc_lat, "%02d%07.4f,%c", abs(deg), min, dir);
char gga_lon[20], rmc_lon[20];
- double lond = cur_fdm_state->get_Longitude() * SGD_RADIANS_TO_DEGREES;
+ double lond = fdm->get_Longitude() * SGD_RADIANS_TO_DEGREES;
if ( lond < 0.0 ) {
lond = -lond;
dir = 'W';
}
deg = (int)(lond);
min = (lond - (double)deg) * 60.0;
- sprintf( gga_lon, "%03d%06.3f,%c", abs(deg), min, dir);
+ sprintf( gga_lon, "%03d%07.4f,%c", abs(deg), min, dir);
sprintf( rmc_lon, "%03d%07.4f,%c", abs(deg), min, dir);
+ double vn = fgGetDouble( "/velocities/speed-north-fps" );
+ double ve = fgGetDouble( "/velocities/speed-east-fps" );
+ double fps = sqrt( vn*vn + ve*ve );
+ double mps = fps * SG_FEET_TO_METER;
+ double kts = mps * SG_METER_TO_NM * 3600;
char speed[10];
- sprintf( speed, "%05.1f", cur_fdm_state->get_V_equiv_kts() );
+ sprintf( speed, "%.1f", kts );
+ double hdg_true = atan2( ve, vn ) * SGD_RADIANS_TO_DEGREES;
+ if ( hdg_true < 0 ) {
+ hdg_true += 360.0;
+ }
char heading[10];
- sprintf( heading, "%05.1f", cur_fdm_state->get_Psi() * SGD_RADIANS_TO_DEGREES );
+ sprintf( heading, "%.1f", hdg_true );
char altitude_m[10];
- sprintf( altitude_m, "%02d",
- (int)(cur_fdm_state->get_Altitude() * SG_FEET_TO_METER) );
+ sprintf( altitude_m, "%.1f",
+ fdm->get_Altitude() * SG_FEET_TO_METER );
char date[10];
int year = t->getGmt()->tm_year;
} else {
dir = 'E';
}
- sprintf( magvar, "%05.1f,%c", magdeg, dir );
+ sprintf( magvar, "%.1f,%c", magdeg, dir );
- // $GPRMC,HHMMSS,A,DDMM.MMMM,N,DDDMM.MMMM,W,XXX.X,XXX.X,DDMMYY,XXX.X,E*XX
- sprintf( rmc, "GPRMC,%s,A,%s,%s,%s,%s,%s,%s",
+ // $GPRMC,HHMMSS,A,DDMM.MMMM,N,DDDMM.MMMM,W,XXX.X,XXX.X,DDMMYY,XXX.X,E,A*XX
+ sprintf( rmc, "GPRMC,%s,A,%s,%s,%s,%s,%s,%s,A",
utc, rmc_lat, rmc_lon, speed, heading, date, magvar );
sprintf( rmc_sum, "%02X", calc_nmea_cksum(rmc) );
- sprintf( gga, "GPGGA,%s,%s,%s,1,08,0.9,%s,M, , ",
+ // $GPGGA,HHMMSS,DDMM.MMMM,N,DDDMM.MMMM,W,1,NN,H.H,AAAA.A,M,GG.G,M,,*XX
+ sprintf( gga, "GPGGA,%s,%s,%s,1,08,0.9,%s,M,0.0,M,,",
utc, gga_lat, gga_lon, altitude_m );
sprintf( gga_sum, "%02X", calc_nmea_cksum(gga) );
sprintf( gsa, "%s",
nmea_sentence += rmc;
nmea_sentence += "*";
nmea_sentence += rmc_sum;
- nmea_sentence += "\r\n";
+ nmea_sentence += "\n";
// GGA sentence
nmea_sentence += "$";
nmea_sentence += gga;
nmea_sentence += "*";
nmea_sentence += gga_sum;
- nmea_sentence += "\r\n";
+ nmea_sentence += "\n";
// GSA sentence (totally faked)
nmea_sentence += gsa;
- nmea_sentence += "\r\n";
+ nmea_sentence += "\n";
-// cout << nmea_sentence;
+ // cout << nmea_sentence;
length = nmea_sentence.length();
strncpy( buf, nmea_sentence.c_str(), length );
lat *= -1;
}
- cur_fdm_state->set_Latitude( lat * SGD_DEGREES_TO_RADIANS );
+ fdm->set_Latitude( lat * SGD_DEGREES_TO_RADIANS );
SG_LOG( SG_IO, SG_INFO, " lat = " << lat );
// lon val
lon *= -1;
}
- cur_fdm_state->set_Longitude( lon * SGD_DEGREES_TO_RADIANS );
+ fdm->set_Longitude( lon * SGD_DEGREES_TO_RADIANS );
SG_LOG( SG_IO, SG_INFO, " lon = " << lon );
#if 0
double sl_radius, lat_geoc;
- sgGeodToGeoc( cur_fdm_state->get_Latitude(),
- cur_fdm_state->get_Altitude(),
+ sgGeodToGeoc( fdm->get_Latitude(),
+ fdm->get_Altitude(),
&sl_radius, &lat_geoc );
- cur_fdm_state->set_Geocentric_Position( lat_geoc,
- cur_fdm_state->get_Longitude(),
- sl_radius + cur_fdm_state->get_Altitude() );
+ fdm->set_Geocentric_Position( lat_geoc,
+ fdm->get_Longitude(),
+ sl_radius + fdm->get_Altitude() );
#endif
// speed
string speed_str = msg.substr(begin, end - begin);
begin = end + 1;
speed = atof( speed_str.c_str() );
- cur_fdm_state->set_V_calibrated_kts( speed );
- // cur_fdm_state->set_V_ground_speed( speed );
+ fdm->set_V_calibrated_kts( speed );
+ // fdm->set_V_ground_speed( speed );
SG_LOG( SG_IO, SG_INFO, " speed = " << speed );
// heading
string hdg_str = msg.substr(begin, end - begin);
begin = end + 1;
heading = atof( hdg_str.c_str() );
- cur_fdm_state->set_Euler_Angles( cur_fdm_state->get_Phi(),
- cur_fdm_state->get_Theta(),
+ fdm->set_Euler_Angles( fdm->get_Phi(),
+ fdm->get_Theta(),
heading * SGD_DEGREES_TO_RADIANS );
SG_LOG( SG_IO, SG_INFO, " heading = " << heading );
} else if ( sentence == "GPGGA" ) {
lat *= -1;
}
- // cur_fdm_state->set_Latitude( lat * SGD_DEGREES_TO_RADIANS );
+ // fdm->set_Latitude( lat * SGD_DEGREES_TO_RADIANS );
SG_LOG( SG_IO, SG_INFO, " lat = " << lat );
// lon val
lon *= -1;
}
- // cur_fdm_state->set_Longitude( lon * SGD_DEGREES_TO_RADIANS );
+ // fdm->set_Longitude( lon * SGD_DEGREES_TO_RADIANS );
SG_LOG( SG_IO, SG_INFO, " lon = " << lon );
// junk
altitude *= SG_METER_TO_FEET;
}
- cur_fdm_state->set_Altitude( altitude );
+ fdm->set_Altitude( altitude );
SG_LOG( SG_IO, SG_INFO, " altitude = " << altitude );
projects / flightgear.git / blobdiff