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C++ NMEAInfo::ProvideNettoVario方法代码示例

本文整理汇总了C++中NMEAInfo::ProvideNettoVario方法的典型用法代码示例。如果您正苦于以下问题：C++ NMEAInfo::ProvideNettoVario方法的具体用法？C++ NMEAInfo::ProvideNettoVario怎么用？C++ NMEAInfo::ProvideNettoVario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::ProvideNettoVario方法的8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: 

// $PDVDS,nx,nz,flap,stallratio,netto
static bool
PDVDS(NMEAInputLine &line, NMEAInfo &info)
{
  fixed AccelX = line.read(fixed_zero);
  fixed AccelZ = line.read(fixed_zero);

  int mag = (int)hypot(AccelX, AccelZ);
  info.acceleration.ProvideGLoad(fixed(mag) / 100, true);

  /*
  double flap = line.read(0.0);
  */
  line.skip();

  info.stall_ratio = line.read(fixed_zero);
  info.stall_ratio_available.Update(info.clock);

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

  //hasVega = true;

  return true;
}
开发者ID:aharrison24，项目名称:XCSoar，代码行数:26，代码来源:Parser.cpp

示例2: 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3: 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4: 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5: 

/**
 * 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6: 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7: 

/**
 * Parse the $PLXVF sentence (LXNav V7).
 *
 * $PLXVF,time ,AccX,AccY,AccZ,Vario,IAS,PressAlt*CS<CR><LF>
 *
 * Example: $PLXVF,1.00,0.87,-0.12,-0.25,90.2,244.3,*CS<CR><LF>
 *
 * @see http://www.xcsoar.org/trac/raw-attachment/ticket/1666/V7%20dataport%20specification%201.97.pdf
 */
static bool
PLXVF(NMEAInputLine &line, NMEAInfo &info)
{
  line.Skip(4);

  fixed vario;
  if (line.ReadChecked(vario))
    info.ProvideNettoVario(vario);

  fixed ias;
  bool have_ias = line.ReadChecked(ias);

  fixed altitude;
  if (line.ReadChecked(altitude)) {
    info.ProvidePressureAltitude(altitude);

    if (have_ias)
      info.ProvideIndicatedAirspeedWithAltitude(ias, altitude);
  }

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

示例8: SmallHypot

// $PDVDS,nx,nz,flap,stallratio,netto
static bool
PDVDS(NMEAInputLine &line, NMEAInfo &info)
{
  const int accel_x = line.Read(0), accel_z = line.Read(0);

  fixed mag = SmallHypot(fixed(accel_x), fixed(accel_z));
  info.acceleration.ProvideGLoad(mag / 100, true);

  /*
  double flap = line.Read(0.0);
  */
  line.Skip();

  info.stall_ratio = line.Read(fixed(0));
  info.stall_ratio_available.Update(info.clock);

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

  //hasVega = true;

  return true;
}
开发者ID:CnZoom，项目名称:XcSoarPull，代码行数:25，代码来源:Parser.cpp


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