#include #include #include #include #include "gps.hxx" SG_USING_STD(cout); SG_USING_STD(endl); GPSTrack::GPSTrack() {}; GPSTrack::~GPSTrack() {}; // load the specified file, return the number of records loaded int GPSTrack::load( const string &file ) { int count = 0; data.clear(); // openg the file sg_gzifstream in( file ); if ( !in.is_open() ) { cout << "Cannot open file: " << file << endl; return 0; } vector tokens; GPSPoint p; while ( ! in.eof() ) { char tmp[2049]; in.getline(tmp, 2048); tokens.clear(); tokens = simgear::strutils::split(tmp, ","); int dd; double raw, min; if ( tokens[0] == "$GPRMC" && tokens.size() == 13 ) { double raw_time = atof(tokens[1].c_str()); GPSTime gps_time = GPSTime( raw_time ); if ( (gps_time.get_time() > p.gps_time.get_time()) && (p.gps_time.get_time() > 1.0) ) { // new data cycle store last data before continuing data.push_back( p ); count++; } p.gps_time = gps_time; raw = atof( tokens[3].c_str() ); dd = (int)(raw / 100.00); min = raw - dd * 100.0; p.lat_deg = dd + min / 60.0; if ( tokens[4] == "S" ) { p.lat_deg = -p.lat_deg; } raw = atof( tokens[5].c_str() ); dd = (int)(raw / 100.00); min = raw - dd * 100.0; p.lon_deg = dd + min / 60.0; if ( tokens[6] == "W" ) { p.lon_deg = -p.lon_deg; } static double max_speed = 0.0; p.speed_kts = atof( tokens[7].c_str() ); if ( p.speed_kts > max_speed ) { max_speed = p.speed_kts; cout << "max speed = " << max_speed << endl; } p.course_true = atof( tokens[8].c_str() ) * SGD_DEGREES_TO_RADIANS; } else if ( tokens[0] == "$GPGGA" && tokens.size() == 15 ) { double raw_time = atof(tokens[1].c_str()); GPSTime gps_time = GPSTime( raw_time ); if ( fabs(gps_time.get_time() - p.gps_time.get_time()) < 0.0001 && (p.gps_time.get_time() > 1.0) ) { // new data cycle store last data before continuing data.push_back( p ); count++; } p.gps_time = gps_time; raw = atof( tokens[2].c_str() ); dd = (int)(raw / 100.00); min = raw - dd * 100.0; p.lat_deg = dd + min / 60.0; if ( tokens[3] == "S" ) { p.lat_deg = -p.lat_deg; } raw = atof( tokens[4].c_str() ); dd = (int)(raw / 100.00); min = raw - dd * 100.0; p.lon_deg = dd + min / 60.0; if ( tokens[5] == "W" ) { p.lon_deg = -p.lon_deg; } p.fix_quality = atoi( tokens[6].c_str() ); p.num_satellites = atoi( tokens[7].c_str() ); p.hdop = atof( tokens[8].c_str() ); static double max_alt = 0.0; double alt = atof( tokens[9].c_str() ); if ( alt > max_alt ) { max_alt = alt; cout << "max alt = " << max_alt << endl; } if ( tokens[10] == "F" || tokens[10] == "f" ) { alt *= SG_FEET_TO_METER; } p.altitude_msl = alt; } } return count; } static double interp( double a, double b, double p, bool rotational = false ) { double diff = b - a; if ( rotational ) { // special handling of rotational data if ( diff > SGD_PI ) { diff -= SGD_2PI; } else if ( diff < -SGD_PI ) { diff += SGD_2PI; } } return a + diff * p; } GPSPoint GPSInterpolate( const GPSPoint A, const GPSPoint B, const double percent ) { GPSPoint p; p.gps_time = GPSTime((int)interp(A.gps_time.get_time(), B.gps_time.get_time(), percent)); p.lat_deg = interp(A.lat_deg, B.lat_deg, percent); p.lon_deg = interp(A.lon_deg, B.lon_deg, percent); p.fix_quality = (int)interp(A.fix_quality, B.fix_quality, percent); p.num_satellites = (int)interp(A.num_satellites, B.num_satellites, percent); p.hdop = interp(A.hdop, B.hdop, percent); p.altitude_msl = interp(A.altitude_msl, B.altitude_msl, percent); p.speed_kts = interp(A.speed_kts, B.speed_kts, percent); p.course_true = interp(A.course_true, B.course_true, percent, true); return p; }