Beispiel #1
0
void
RenderMacCready(Canvas &canvas, const PixelRect rc,
                 const ChartLook &chart_look,
                 const GlidePolar &glide_polar)
{
  ChartRenderer chart(chart_look, canvas, rc);

  if (!glide_polar.IsValid()) {
    chart.DrawNoData();
    return;
  }

  chart.ScaleXFromValue(0);
  chart.ScaleXFromValue(MAX_MACCREADY);
  chart.ScaleYFromValue(0);
  chart.ScaleYFromValue(glide_polar.GetVMax());

  chart.DrawXGrid(Units::ToSysVSpeed(1), 1, ChartRenderer::UnitFormat::NUMERIC);
  chart.DrawYGrid(Units::ToSysSpeed(10), 10, ChartRenderer::UnitFormat::NUMERIC);

  GlidePolar gp = glide_polar;
  double m = 0;
  double m_last;
  gp.SetMC(m);
  double v_last = gp.GetVBestLD();
  double vav_last = 0;
  do {
    m_last = m;
    m+= MAX_MACCREADY/STEPS_MACCREADY;
    gp.SetMC(m);
    const double v = gp.GetVBestLD();
    const double vav = gp.GetAverageSpeed();
    chart.DrawLine(m_last, v_last, m, v, ChartLook::STYLE_BLACK);
    chart.DrawLine(m_last, vav_last, m, vav, ChartLook::STYLE_BLUETHINDASH);
    v_last = v;
    vav_last = vav;
  } while (m<MAX_MACCREADY);

  // draw current MC setting
  chart.DrawLine(glide_polar.GetMC(), 0, glide_polar.GetMC(), glide_polar.GetVMax(),
                 ChartLook::STYLE_REDTHICKDASH);

  // draw labels and other overlays

  gp.SetMC(0.9*MAX_MACCREADY);
  chart.DrawLabel(_T("Vopt"), 0.9*MAX_MACCREADY, gp.GetVBestLD());
  gp.SetMC(0.9*MAX_MACCREADY);
  chart.DrawLabel(_T("Vave"), 0.9*MAX_MACCREADY, gp.GetAverageSpeed());

  chart.DrawYLabel(_T("V"), Units::GetSpeedName());
  chart.DrawXLabel(_T("MC"), Units::GetVerticalSpeedName());

  RenderGlidePolarInfo(canvas, rc, chart_look, glide_polar);
}
Beispiel #2
0
void
GlidePolarTest::TestBasic()
{
  polar.Update();

  ok1(equals(polar.polar.a, polar.ideal_polar.a));
  ok1(equals(polar.polar.b, polar.ideal_polar.b));
  ok1(equals(polar.polar.c, polar.ideal_polar.c));

  ok1(equals(polar.SinkRate(Units::ToSysUnit(fixed(80), Unit::KILOMETER_PER_HOUR)), 0.606));
  ok1(equals(polar.SinkRate(Units::ToSysUnit(fixed(120), Unit::KILOMETER_PER_HOUR)), 0.99));
  ok1(equals(polar.SinkRate(Units::ToSysUnit(fixed(160), Unit::KILOMETER_PER_HOUR)), 1.918));

  ok1(equals(polar.GetSMax(), polar.SinkRate(polar.GetVMax())));

  ok1(equals(polar.GetVMin(), 19.934640523));
  ok1(equals(polar.GetSMin(), polar.SinkRate(polar.GetVMin())));
  ok1(equals(polar.GetVTakeoff(), polar.GetVMin() / 2));

  ok1(equals(polar.GetVBestLD(), 25.830434162));
  ok1(equals(polar.GetSBestLD(), polar.SinkRate(polar.GetVBestLD())));
  ok1(equals(polar.GetBestLD(), polar.GetVBestLD() / polar.GetSBestLD()));

  ok1(equals(polar.GetTotalMass(), 318));
  ok1(equals(polar.GetWingLoading(), 32.448979592));
  ok1(equals(polar.GetBallast(), 0));
  ok1(equals(polar.GetBallastLitres(), 0));
  ok1(polar.IsBallastable());
  ok1(!polar.HasBallast());
}
bool 
AirspaceWarningManager::UpdateTask(const AircraftState &state,
                                   const GlidePolar &glide_polar,
                                   const TaskStats &task_stats)
{
  if (!glide_polar.IsValid())
    return false;

  const ElementStat &current_leg = task_stats.current_leg;

  if (!task_stats.task_valid || !current_leg.location_remaining.IsValid())
    return false;

  const GlideResult &solution = current_leg.solution_remaining;
  if (!solution.IsOk() || !solution.IsAchievable())
    /* glide solver failed, cannot continue */
    return false;

  const AirspaceAircraftPerformance perf_task(glide_polar,
                                              current_leg.solution_remaining);
  GeoPoint location_tp = current_leg.location_remaining;
  const fixed time_remaining = solution.time_elapsed;

  const GeoVector vector(state.location, location_tp);
  fixed max_distance = config.warning_time * glide_polar.GetVMax();
  if (vector.distance > max_distance)
    /* limit the distance to what our glider can actually fly within
       the configured warning time */
    location_tp = state.location.IntermediatePoint(location_tp, max_distance);

  return UpdatePredicted(state, location_tp, perf_task,
                          AirspaceWarning::WARNING_TASK, time_remaining);
}
 /**
  * Specialisation based on simplified theoretical MC cross-country
  * speeds.  Assumes cruise at best LD (ignoring wind) for current MC
  * setting, climb rate at MC setting, with direct descent possible
  * at sink rate of cruise.
  */
 explicit AirspaceAircraftPerformance(const GlidePolar &polar)
   :vertical_tolerance(0),
    cruise_speed(polar.GetVBestLD()), cruise_descent(polar.GetSBestLD()),
    descent_rate(polar.GetSMax()),
    climb_rate(polar.GetMC()),
    max_speed(polar.GetVMax()) {
   assert(polar.IsValid());
 }