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C++ NMEAInfo::ProvideTotalEnergyVario方法代码示例

本文整理汇总了C++中NMEAInfo::ProvideTotalEnergyVario方法的典型用法代码示例。如果您正苦于以下问题：C++ NMEAInfo::ProvideTotalEnergyVario方法的具体用法？C++ NMEAInfo::ProvideTotalEnergyVario怎么用？C++ NMEAInfo::ProvideTotalEnergyVario使用的例子？那么, 这里精选的方法代码示例或许可以为您提供帮助。您也可以进一步了解该方法所在类NMEAInfo的用法示例。


在下文中一共展示了NMEAInfo::ProvideTotalEnergyVario方法的15个代码示例，这些例子默认根据受欢迎程度排序。您可以为喜欢或者感觉有用的代码点赞，您的评价将有助于系统推荐出更棒的C++代码示例。

示例1: while

bool
OpenVarioDevice::POV(NMEAInputLine &line, NMEAInfo &info)
{
  /*
   * Type definitions:
   *
   * E: TE vario in m/s
   * P: static pressure in hPa
   * Q: dynamic pressure in Pa
   * R: total pressure in hPa
   * S: true airspeed in km/h
   * T: temperature in deg C
   */

  while (!line.IsEmpty()) {
    char type = line.ReadOneChar();
    if (type == '\0')
      break;

    fixed value;
    if (!line.ReadChecked(value))
      break;

    switch (type) {
      case 'E': {
        info.ProvideTotalEnergyVario(value);
        break;
      }
      case 'P': {
        AtmosphericPressure pressure = AtmosphericPressure::HectoPascal(value);
        info.ProvideStaticPressure(pressure);
        break;
      }
      case 'Q': {
        AtmosphericPressure pressure = AtmosphericPressure::Pascal(value);
        info.ProvideDynamicPressure(pressure);
        break;
      }
      case 'R': {
        AtmosphericPressure pressure = AtmosphericPressure::HectoPascal(value);
        info.ProvidePitotPressure(pressure);
        break;
      }
      case 'S': {
        value = Units::ToSysUnit(value, Unit::KILOMETER_PER_HOUR);
        info.ProvideTrueAirspeed(value);
        break;
      }
      case 'T': {
        info.temperature = CelsiusToKelvin(value);
        info.temperature_available = true;
        break;
      }
    }
  }

  return true;
}
开发者ID:kwtskran，项目名称:XCSoar，代码行数:58，代码来源:OpenVario.cpp

示例2: 

static bool
ParsePITV4(NMEAInputLine &line, NMEAInfo &info)
{
  fixed value;

  // TE vario [m/s]
  if (line.ReadChecked(value))
    info.ProvideTotalEnergyVario(value);

  return true;
}
开发者ID:CnZoom，项目名称:XcSoarPull，代码行数:11，代码来源:Vaulter.cpp

示例3: fixed

static bool
PZAN2(NMEAInputLine &line, NMEAInfo &info)
{
  fixed vtas, wnet;

  if (line.ReadChecked(vtas))
    info.ProvideTrueAirspeed(Units::ToSysUnit(vtas, Unit::KILOMETER_PER_HOUR));

  if (line.ReadChecked(wnet))
    info.ProvideTotalEnergyVario((wnet - fixed(10000)) / 100);

  return true;
}
开发者ID:CnZoom，项目名称:XcSoarPull，代码行数:13，代码来源:Zander.cpp

示例4: if

/**
 * $PWES0,DD,VVVV,MMMM,NNNN,BBBB,SSSS,AAAAA,QQQQQ,IIII,TTTT,UUU,CCCC*CS<CR><LF>
 */
static bool
PWES0(NMEAInputLine &line, NMEAInfo &info)
{
  int i;

  line.Skip(); /* device */

  if (line.ReadChecked(i) && i >= -999 && i <= 999)
    info.ProvideTotalEnergyVario(fixed(i) / 10);

  line.Skip(); /* average vario */

  if (line.ReadChecked(i) && i >= -999 && i <= 999)
    info.ProvideNettoVario(fixed(i) / 10);

  line.Skip(); /* average netto vario */
  line.Skip(); /* speed to fly */

  unsigned altitude;
  if (line.ReadChecked(altitude) && altitude <= 99999)
    info.ProvidePressureAltitude(fixed(altitude));

  if (line.ReadChecked(altitude) && altitude <= 99999)
    info.ProvideBaroAltitudeTrue(fixed(altitude));

  unsigned ias, tas;
  bool have_ias = line.ReadChecked(ias) && ias <= 9999;
  bool have_tas = line.ReadChecked(tas) && tas <= 9999;
  if (have_ias && have_tas)
    info.ProvideBothAirspeeds(Units::ToSysUnit(fixed(ias) / 10,
                                               Unit::KILOMETER_PER_HOUR),
                              Units::ToSysUnit(fixed(tas) / 10,
                                               Unit::KILOMETER_PER_HOUR));

  else if (!have_ias && have_tas)
    info.ProvideTrueAirspeed(Units::ToSysUnit(fixed(tas) / 10,
                                              Unit::KILOMETER_PER_HOUR));

  unsigned voltage;
  if (line.ReadChecked(voltage) && voltage <= 999) {
    info.voltage = fixed(voltage) / 10;
    info.voltage_available.Update(info.clock);
  }

  if (line.ReadChecked(i) && i >= -999 && i <= 999) {
    info.temperature = CelsiusToKelvin(fixed(i) / 10);
    info.temperature_available = true;
  }

  return true;
}
开发者ID:CnZoom，项目名称:XcSoarPull，代码行数:54，代码来源:Westerboer.cpp

示例5: if

/**
 * $PWES0,DD,VVVV,MMMM,NNNN,BBBB,SSSS,AAAAA,QQQQQ,IIII,TTTT,UUU,CCCC*CS<CR><LF>
 */
static bool
PWES0(NMEAInputLine &line, NMEAInfo &info)
{
  int i, k;

  line.skip(); /* device */

  if (line.read_checked(i))
    info.ProvideTotalEnergyVario(fixed(i) / 10);

  line.skip(); /* average vario */

  if (line.read_checked(i))
    info.ProvideNettoVario(fixed(i) / 10);

  line.skip(); /* average netto vario */
  line.skip(); /* speed to fly */

  if (line.read_checked(i))
    info.ProvidePressureAltitude(fixed(i));

  if (line.read_checked(i))
    info.ProvideBaroAltitudeTrue(fixed(i));

  bool have_ias = line.read_checked(i);
  bool have_tas = line.read_checked(k);
  if (have_ias && have_tas)
    info.ProvideBothAirspeeds(Units::ToSysUnit(fixed(i) / 10,
                                               Unit::KILOMETER_PER_HOUR),
                              Units::ToSysUnit(fixed(k) / 10,
                                               Unit::KILOMETER_PER_HOUR));

  else if (!have_ias && have_tas)
    info.ProvideTrueAirspeed(Units::ToSysUnit(fixed(k) / 10,
                                              Unit::KILOMETER_PER_HOUR));

  if (line.read_checked(i)) {
    info.voltage = fixed(i) / 10;
    info.voltage_available.Update(info.clock);
  }

  if (line.read_checked(i)) {
    info.temperature = CelsiusToKelvin(fixed(i) / 10);
    info.temperature_available = true;
  }

  return true;
}
开发者ID:davidswelt，项目名称:XCSoar，代码行数:51，代码来源:Westerboer.cpp

示例6: IAS

static bool
LXWP0(NMEAInputLine &line, NMEAInfo &info)
{
  /*
  $LXWP0,Y,222.3,1665.5,1.71,,,,,,239,174,10.1

   0 loger_stored (Y/N)
   1 IAS (kph) ----> Condor uses TAS!
   2 baroaltitude (m)
   3-8 vario (m/s) (last 6 measurements in last second)
   9 heading of plane
  10 windcourse (deg)
  11 windspeed (kph)
  */

  line.Skip();

  fixed airspeed;
  bool tas_available = line.ReadChecked(airspeed);
  if (tas_available && (airspeed < fixed(-50) || airspeed > fixed(250)))
    /* implausible */
    return false;

  fixed value;
  if (line.ReadChecked(value))
    /* a dump on a LX7007 has confirmed that the LX sends uncorrected
       altitude above 1013.25hPa here */
    info.ProvidePressureAltitude(value);

  if (tas_available)
    /*
     * Call ProvideTrueAirspeed() after ProvidePressureAltitude() to use
     * the provided altitude (if available)
     */
    info.ProvideTrueAirspeed(Units::ToSysUnit(airspeed, Unit::KILOMETER_PER_HOUR));

  if (line.ReadChecked(value))
    info.ProvideTotalEnergyVario(value);

  line.Skip(6);

  SpeedVector wind;
  if (ReadSpeedVector(line, wind))
    info.ProvideExternalWind(wind);

  return true;
}
开发者ID:kwtskran，项目名称:XCSoar，代码行数:47，代码来源:Parser.cpp

示例7: CelsiusToKelvin

/**
 * Parse a "$D" sentence.
 *
 * Example: "$D,+0,100554,+25,18,+31,,0,-356,+25,+11,115,96*6A"
 */
static bool
LeonardoParseD(NMEAInputLine &line, NMEAInfo &info)
{
  double value;

  // 0 = vario [dm/s]
  if (line.ReadChecked(value))
    info.ProvideTotalEnergyVario(value / 10);

  if (line.Rest().empty())
    /* short "$D" sentence ends after vario */
    return true;

  // 1 = air pressure [Pa]
  if (line.ReadChecked(value))
    info.ProvideStaticPressure(AtmosphericPressure::Pascal(value));

  // 2 = netto vario [dm/s]
  if (line.ReadChecked(value))
    info.ProvideNettoVario(value / 10);

  // 3 = airspeed [km/h]
  /* XXX is that TAS or IAS? */
  if (line.ReadChecked(value))
    info.ProvideTrueAirspeed(Units::ToSysUnit(value, Unit::KILOMETER_PER_HOUR));

  // 4 = temperature [deg C]
  double oat;
  info.temperature_available = line.ReadChecked(oat);
  if (info.temperature_available)
    info.temperature = CelsiusToKelvin(oat);

  // 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;
}
开发者ID:MaxPower-No1，项目名称:XCSoar，代码行数:52，代码来源:Leonardo.cpp

示例8: fixed

bool
NMEAParser::PTAS1(NMEAInputLine &line, NMEAInfo &info)
{
    /*
     * $PTAS1,xxx,yyy,zzzzz,aaa*CS<CR><LF>
     *
     * xxx
     * CV or current vario. =vario*10+200 range 0-400(display +/-20.0 knots)
     *
     * yyy
     * AV or average vario. =vario*10+200 range 0-400(display +/-20.0 knots)
     *
     * zzzzz
     * Barometric altitude in feet +2000
     *
     * aaa
     * TAS knots 0-200
     */

    // Parse current vario data
    fixed vario;
    if (line.ReadChecked(vario)) {
        // Properly convert to m/s
        vario = Units::ToSysUnit((vario - fixed(200)) / 10, Unit::KNOTS);
        info.ProvideTotalEnergyVario(vario);
    }

    // Skip average vario data
    line.Skip();

    // Parse barometric altitude
    fixed baro_altitude;
    if (line.ReadChecked(baro_altitude)) {
        // Properly convert to meter
        baro_altitude = Units::ToSysUnit(baro_altitude - fixed(2000), Unit::FEET);
        info.ProvidePressureAltitude(baro_altitude);
    }

    // Parse true airspeed
    fixed vtas;
    if (line.ReadChecked(vtas))
        info.ProvideTrueAirspeed(Units::ToSysUnit(vtas, Unit::KNOTS));

    return true;
}
开发者ID:ThomasXBMC，项目名称:XCSoar，代码行数:45，代码来源:Parser.cpp

示例9: 

/**
 * Parse a "$PDGFTL1" sentence.
 *
 * Example: "$PDGFTL1,2025,2000,250,-14,45,134,28,65,382,153*3D"
 */
static bool
PDGFTL1(NMEAInputLine &line, NMEAInfo &info)
{
  double value;

  //  Baro Altitude QNE(1013.25)     2025     meter        2025 mt
  if (line.ReadChecked(value))
    info.ProvidePressureAltitude(value);

  //  Baro Altitude QNH  2000     meter        2000 mt
  if (line.ReadChecked(value))
    info.ProvideBaroAltitudeTrue(value);

  //  Vario  250      cm/sec       +2,50 m/s
  if (line.ReadChecked(value))
    info.ProvideTotalEnergyVario(value / 100);

  //  Netto Vario  -14      dm/sec       -1,40 m/s
  if (line.ReadChecked(value))
    info.ProvideNettoVario(value / 10);

  //  Indicated Air Speed  45       km/h         45 km/h
  if (line.ReadChecked(value))
    info.ProvideIndicatedAirspeed(Units::ToSysUnit(value, Unit::KILOMETER_PER_HOUR));

  //  Ground Efficiency  134      ratio        13,4 : 1
  line.Skip();

  //  Wind Speed  28       km/h         28 km/h
  //  Wind Direction  65       degree       65 degree
  SpeedVector wind;
  if (ReadSpeedVector(line, wind))
    info.ProvideExternalWind(wind);

  //  Main Lithium Battery Voltage   382      0.01 volts   3,82 volts
  if (line.ReadChecked(value)) {
    info.voltage = value / 100;
    info.voltage_available.Update(info.clock);
  }

  //  Backup AA Battery Voltage      153      0.01 volts   1,53 volts

  return true;
}
开发者ID:MaxPower-No1，项目名称:XCSoar，代码行数:49，代码来源:Leonardo.cpp

示例10: IAS

static bool
cLXWP0(NMEAInputLine &line, NMEAInfo &info)
{
  /*
  $LXWP0,Y,222.3,1665.5,1.71,,,,,,239,174,10.1

   0 logger_stored (Y/N)
   1 IAS (kph) ----> Condor uses TAS!
   2 baroaltitude (m)
   3 vario (m/s)
   4-8 unknown
   9 heading of plane
  10 windcourse (deg)
  11 windspeed (kph)
  */

  fixed value;

  line.Skip();

  fixed airspeed;
  bool tas_available = line.ReadChecked(airspeed);

  fixed alt = line.Read(fixed_zero);

  if (tas_available)
    info.ProvideTrueAirspeedWithAltitude(Units::ToSysUnit(airspeed,
                                                               Unit::KILOMETER_PER_HOUR),
                                              alt);

  // ToDo check if QNH correction is needed!
  info.ProvideBaroAltitudeTrue(alt);

  if (line.ReadChecked(value))
    info.ProvideTotalEnergyVario(value);

  line.Skip(6);

  SpeedVector wind;
  if (ReadSpeedVector(line, wind))
    info.ProvideExternalWind(wind);

  return true;
}
开发者ID:alon，项目名称:xcsoar，代码行数:44，代码来源:Condor.cpp

示例11: fixed

/**
 * $PWES0,DD,VVVV,MMMM,NNNN,BBBB,SSSS,AAAAA,QQQQQ,IIII,TTTT,UUU,CCC*CS<CR><LF>
 */
static bool
PWES0(NMEAInputLine &line, NMEAInfo &info)
{
    int i, k;

    line.skip(); /* device */

    if (line.read_checked(i))
        info.ProvideTotalEnergyVario(fixed(i) / 10);

    line.skip(); /* average vario */

    if (line.read_checked(i))
        info.ProvideNettoVario(fixed(i) / 10);

    line.skip(); /* average netto vario */
    line.skip(); /* speed to fly */

    if (line.read_checked(i))
        info.ProvidePressureAltitude(fixed(i));

    if (line.read_checked(i))
        info.ProvideBaroAltitudeTrue(fixed(i));

    bool have_ias = line.read_checked(i);
    bool have_tas = line.read_checked(k);
    if (have_ias && have_tas)
        info.ProvideBothAirspeeds(Units::ToSysUnit(fixed(i) / 10,
                                  unKiloMeterPerHour),
                                  Units::ToSysUnit(fixed(k) / 10,
                                          unKiloMeterPerHour));

    if (line.read_checked(i)) {
        info.voltage = fixed(i) / 10;
        info.voltage_available.Update(info.clock);
    }

    if (line.read_checked(i)) {
        info.temperature = Units::ToSysUnit(fixed(i) / 10, unGradCelcius);
        info.temperature_available = true;
    }

    return true;
}
开发者ID:macsux，项目名称:XCSoar，代码行数:47，代码来源:Westerboer.cpp

示例12: 

static bool
PDVDV(NMEAInputLine &line, NMEAInfo &info)
{
  fixed value;

  if (line.read_checked(value))
    info.ProvideTotalEnergyVario(value / 10);

  bool ias_available = line.read_checked(value);
  fixed tas_ratio = line.read(fixed(1024)) / 1024;
  if (ias_available)
    info.ProvideBothAirspeeds(value / 10, value / 10 * tas_ratio);

  //hasVega = true;

  if (line.read_checked(value))
    info.ProvidePressureAltitude(value);

  return true;
}
开发者ID:aharrison24，项目名称:XCSoar，代码行数:20，代码来源:Parser.cpp

示例13: fixed

/**
 * Parses a PTAS1 sentence (Tasman Instruments proprietary).
 *
 * @param String Input string
 * @param params Parameter array
 * @param nparams Number of parameters
 * @param info NMEA_INFO struct to parse into
 * @return Parsing success
 */
bool
NMEAParser::PTAS1(NMEAInputLine &line, NMEAInfo &info)
{
  fixed wnet;
  if (line.read_checked(wnet))
    info.ProvideTotalEnergyVario(Units::ToSysUnit((wnet - fixed(200)) / 10,
                                                       unKnots));

  line.skip(); // average vario +200

  fixed baralt;
  if (line.read_checked(baralt)) {
    baralt = max(fixed_zero, Units::ToSysUnit(baralt - fixed(2000), unFeet));
    info.ProvidePressureAltitude(baralt);
  }

  fixed vtas;
  if (line.read_checked(vtas))
    info.ProvideTrueAirspeed(Units::ToSysUnit(vtas, unKnots));

  return true;
}
开发者ID:macsux，项目名称:XCSoar，代码行数:31，代码来源:Parser.cpp

示例14: fixed

/*
!w,<1>,<2>,<3>,<4>,<5>,<6>,<7>,<8>,<9>,<10>,<11>,<12>,<13>*hh<CR><LF>
<1>  Vector wind direction in degrees
<2>  Vector wind speed in 10ths of meters per second
<3>  Vector wind age in seconds
<4>  Component wind in 10ths of Meters per second + 500 (500 = 0, 495 = 0.5 m/s tailwind)
<5>  True altitude in Meters + 1000
<6>  Instrument QNH setting
<7>  True airspeed in 100ths of Meters per second
<8>  Variometer reading in 10ths of knots + 200
<9>  Averager reading in 10ths of knots + 200
<10> Relative variometer reading in 10ths of knots + 200
<11> Instrument MacCready setting in 10ths of knots
<12> Instrument Ballast setting in percent of capacity
<13> Instrument Bug setting
*hh  Checksum, XOR of all bytes
*/
static bool
cai_w(NMEAInputLine &line, NMEAInfo &info)
{
  SpeedVector wind;
  if (ReadSpeedVector(line, wind))
    info.ProvideExternalWind(wind.Reciprocal());

  line.skip(2);

  fixed value;
  if (line.read_checked(value))
    info.ProvideBaroAltitudeTrue(value - fixed(1000));

  if (line.read_checked(value))
    info.settings.ProvideQNH(value, info.clock);

  if (line.read_checked(value))
    info.ProvideTrueAirspeed(value / 100);

  if (line.read_checked(value))
    info.ProvideTotalEnergyVario(Units::ToSysUnit((value - fixed(200)) / 10,
                                                  unKnots));

  line.skip(2);

  int i;

  if (line.read_checked(i))
    info.settings.ProvideMacCready(Units::ToSysUnit(fixed(i) / 10, unKnots),
                                   info.clock);

  if (line.read_checked(i))
    info.settings.ProvideBallastFraction(fixed(i) / 100, info.clock);

  if (line.read_checked(i))
    info.settings.ProvideBugs(fixed(i) / 100, info.clock);

  return true;
}
开发者ID:macsux，项目名称:XCSoar，代码行数:56，代码来源:Parser.cpp

示例15: fixed

static bool
PDVDV(NMEAInputLine &line, NMEAInfo &info)
{
  int value;

  if (line.ReadChecked(value))
    info.ProvideTotalEnergyVario(fixed(value) / 10);

  bool ias_available = line.ReadChecked(value);
  int tas_ratio = line.Read(1024);
  if (ias_available) {
    const fixed ias = fixed(value) / 10;
    info.ProvideBothAirspeeds(ias, ias * tas_ratio / 1024);
  }

  //hasVega = true;

  if (line.ReadChecked(value))
    info.ProvidePressureAltitude(fixed(value));

  return true;
}
开发者ID:CnZoom，项目名称:XcSoarPull，代码行数:22，代码来源:Parser.cpp


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