/**
* Parse a "$VMVABD" sentence.
*
* Example: "$VMVABD,0000.0,M,0547.0,M,-0.0,,,MS,0.0,KH,22.4,C*65"
*/
static bool
FlytecParseVMVABD(NMEAInputLine &line, NMEA_INFO &info)
{
fixed value;
// 0,1 = GPS altitude, unit
if (line.read_checked_compare(info.GPSAltitude, "M"))
info.GPSAltitudeAvailable.Update(info.clock);
// 2,3 = baro altitude, unit
if (line.read_checked_compare(value, "M"))
info.ProvideBaroAltitudeTrue(value);
// 4-7 = integrated vario, unit
line.skip(4);
// 8,9 = indicated or true airspeed, unit
if (line.read_checked_compare(value, "KH"))
// XXX is that TAS or IAS? Documentation isn't clear.
info.ProvideBothAirspeeds(Units::ToSysUnit(value, unKiloMeterPerHour));
// 10,11 = temperature, unit
info.TemperatureAvailable =
line.read_checked_compare(value, "C");
if (info.TemperatureAvailable)
info.OutsideAirTemperature = Units::ToSysUnit(value, unGradCelcius);
return true;
}
/**
* Update the measurements if new level reached
* @param basic NMEA_INFO for temperature and humidity
*/
void
CuSonde::updateMeasurements(const NMEA_INFO &basic)
{
// if (not flying) nothing to update...
if (!basic.flight.Flying)
return;
// if (no temperature or humidity available) nothing to update...
if (!basic.TemperatureAvailable || !basic.HumidityAvailable)
return;
// find appropriate level
unsigned short level = (unsigned short)((int)max(basic.GetAltitudeBaroPreferred(),
fixed(0.0))
/ CUSONDE_HEIGHTSTEP);
// if (level out of range) cancel update
if (level >= CUSONDE_NUMLEVELS)
return;
// if (level skipped) cancel update
if (abs(level - last_level) > 1) {
last_level = level;
return;
}
// if (no level transition yet) wait for transition
if (abs(level - last_level) == 0)
return;
// calculate ground height
hGround = basic.AltitudeAGL;
// if (going up)
if (level > last_level) {
// we round down (level) because of potential lag of temp sensor
cslevels[level].updateTemps(basic.RelativeHumidity,
Units::ToUserUnit(basic.OutsideAirTemperature, unGradCelcius));
cslevels[level].updateThermalIndex(level);
if (level > 0) {
findThermalHeight((unsigned short)(level - 1));
findCloudBase((unsigned short)(level - 1));
}
// if (going down)
} else {
// we round up (level+1) because of potential lag of temp sensor
cslevels[level + 1].updateTemps(basic.RelativeHumidity,
Units::ToUserUnit(basic.OutsideAirTemperature, unGradCelcius));
cslevels[level + 1].updateThermalIndex((unsigned short)(level + 1));
if (level < CUSONDE_NUMLEVELS - 1) {
findThermalHeight(level);
findCloudBase(level);
}
}
last_level = level;
}
bool
EWMicroRecorderDevice::ParseNMEA(const char *String, NMEA_INFO &info)
{
if (!VerifyNMEAChecksum(String))
return false;
NMEAInputLine line(String);
char type[16];
line.read(type, 16);
if (strcmp(type, "$PGRMZ") == 0) {
fixed value;
/* The normal Garmin $PGRMZ line contains the "true" barometric
altitude above MSL (corrected with QNH), but EWMicroRecorder
differs here slightly: it emits the uncorrected barometric
altitude. That is the only reason why we catch this sentence
in the driver instead of letting the generic class NMEAParser
do it. */
if (ReadAltitude(line, value))
info.ProvidePressureAltitude(value);
return true;
} else
return false;
}
/**
* Parse a "$D" sentence.
*
* Example: "$D,+0,100554,+25,18,+31,,0,-356,+25,+11,115,96*6A"
*/
static bool
LeonardoParseD(NMEAInputLine &line, NMEA_INFO &info)
{
fixed value;
// 0 = vario [dm/s]
if (line.read_checked(value))
info.ProvideTotalEnergyVario(value / 10);
// 1 = air pressure [Pa]
if (line.skip() == 0)
/* short "$C" sentence ends after airspeed */
return true;
// 2 = netto vario [dm/s]
if (line.read_checked(value))
info.ProvideNettoVario(value / 10);
// 3 = airspeed [km/h]
/* XXX is that TAS or IAS? */
if (line.read_checked(value))
info.ProvideTrueAirspeed(Units::ToSysUnit(value, unKiloMeterPerHour));
// 4 = temperature [deg C]
fixed oat;
info.TemperatureAvailable = line.read_checked(oat);
if (info.TemperatureAvailable)
info.OutsideAirTemperature = Units::ToSysUnit(oat, unGradCelcius);
// 5 = compass [degrees]
/* XXX unsupported by XCSoar */
// 6 = optimal speed [km/h]
/* XXX unsupported by XCSoar */
// 7 = equivalent MacCready [cm/s]
/* XXX unsupported by XCSoar */
// 8 = wind speed [km/h]
/* not used here, the "$C" record repeats it together with the
direction */
return true;
}
/**
* Parse a "$C" sentence.
*
* Example: "$C,+2025,-7,+18,+25,+29,122,314,314,0,-356,+25,45,T*3D"
*/
static bool
LeonardoParseC(NMEAInputLine &line, NMEA_INFO &info)
{
fixed value;
// 0 = altitude [m]
if (line.read_checked(value))
info.ProvideBaroAltitudeTrue(value);
// 1 = vario [dm/s]
if (line.read_checked(value))
info.ProvideTotalEnergyVario(value / 10);
// 2 = airspeed [km/h]
/* XXX is that TAS or IAS? */
if (line.read_checked(value))
info.ProvideTrueAirspeed(Units::ToSysUnit(value, unKiloMeterPerHour));
// 3 = netto vario [dm/s]
if (line.read_checked(value))
info.ProvideNettoVario(value / 10);
else
/* short "$C" sentence ends after airspeed */
return true;
// 4 = temperature [deg C]
fixed oat;
info.TemperatureAvailable = line.read_checked(oat);
if (info.TemperatureAvailable)
info.OutsideAirTemperature = Units::ToSysUnit(oat, unGradCelcius);
// 10 = wind speed [km/h]
// 11 = wind direction [degrees]
SpeedVector wind;
if (ReadSpeedVector(line, wind))
info.ProvideExternalWind(wind);
return true;
}
/**
* Parse a "$BRSF" sentence.
*
* Example: "$BRSF,063,-013,-0035,1,193,00351,535,485*38"
*/
static bool
FlytecParseBRSF(NMEAInputLine &line, NMEA_INFO &info)
{
fixed value;
// 0 = indicated or true airspeed [km/h]
if (line.read_checked(value))
// XXX is that TAS or IAS? Documentation isn't clear.
info.ProvideBothAirspeeds(Units::ToSysUnit(value, unKiloMeterPerHour));
// 1 = integrated vario [dm/s]
// 2 = altitude A2 [m] (XXX what's this?)
// 3 = waypoint
// 4 = bearing to waypoint [degrees]
// 5 = distance to waypoint [100m]
// 6 = MacCready speed to fly [100m/h]
// 7 = speed to fly, best glide [100m/h]
return true;
}
/**
* Parse a "$FLYSEN" sentence.
*
* @see http://www.flytec.ch/public/Special%20NMEA%20sentence.pdf
*/
static bool
FlytecParseFLYSEN(NMEAInputLine &line, NMEA_INFO &info)
{
fixed value;
// Time(hhmmss), 6 Digits
line.skip();
// Latitude(ddmm.mmm), 8 Digits incl. decimal
// N (or S), 1 Digit
line.skip(2);
// Longitude(dddmm.mmm), 9 Digits inc. decimal
// E (or W), 1 Digit
line.skip(2);
// Track (xxx Deg), 3 Digits
// Speed over Ground (xxxxx cm/s) 5 Digits
// GPS altitude (xxxxx meter), 5 Digits
line.skip(3);
// Validity of 3 D fix A or V, 1 Digit
char validity = line.read_first_char();
if (validity != 'A' && validity != 'V') {
validity = line.read_first_char();
if (validity != 'A' && validity != 'V')
return false;
}
// Satellites in Use (0 to 12), 2 Digits
line.skip();
// Raw pressure (xxxxxx Pa), 6 Digits
if (line.read_checked(value))
info.ProvideStaticPressure(value / 100);
// Baro Altitude (xxxxx meter), 5 Digits (-xxxx to xxxxx) (Based on 1013.25hPa)
if (line.read_checked(value))
info.ProvidePressureAltitude(value);
// Variometer (xxxx cm/s), 4 or 5 Digits (-9999 to 9999)
if (line.read_checked(value))
info.ProvideTotalEnergyVario(value / 100);
// true airspeed (xxxxx cm/s), 5 Digits (0 to 99999cm/s = 3600km/h)
if (line.read_checked(value))
info.ProvideTrueAirspeed(value / 100);
// Airspeed source P or V, 1 Digit P= pitot, V = Vane wheel
// Temp. PCB (xxx °C), 3 Digits
// Temp. Balloon Envelope (xxx °C), 3 Digits
// Battery Capacity Bank 1 (0 to 100%) 3 Digits
// Battery Capacity Bank 2 (0 to 100%) 3 Digits
// Dist. to WP (xxxxxx m), 6 Digits (Max 200000m)
// Bearing (xxx Deg), 3 Digits
// Speed to fly1 (MC0 xxxxx cm/s), 5 Digits
// Speed to fly2 (McC. xxxxx cm/s) 5 Digits
// Keypress Code (Experimental empty to 99) 2 Digits
return true;
}
