示例#1
0
static Window *
OnCreateCrossSectionControl(ContainerWindow &parent, PixelRect rc,
                            const WindowStyle style)
{
  csw = new CrossSectionControl(look->cross_section, look->map.airspace,
                                look->chart);
  csw->Create(parent, rc, style);
  csw->SetAirspaces(airspaces);
  csw->SetTerrain(terrain);
  UpdateCrossSection();
  return csw;
}
示例#2
0
static Window *
OnCreateCrossSectionControl(ContainerWindow &parent, int left, int top,
                            unsigned width, unsigned height,
                            const WindowStyle style)
{
    csw = new CrossSectionControl(look->cross_section, look->airspace,
                                  look->chart);
    csw->set(parent, left, top, width, height, style);
    csw->set_airspaces(airspaces);
    csw->set_terrain(terrain);
    UpdateCrossSection();
    return csw;
}
示例#3
0
static Window *
OnCreateCrossSectionControl(ContainerWindow &parent,
                            PixelScalar left, PixelScalar top,
                            UPixelScalar width, UPixelScalar height,
                            const WindowStyle style)
{
  csw = new CrossSectionControl(look->cross_section, look->map.airspace,
                                look->chart);
  csw->set(parent, left, top, width, height, style);
  csw->set_airspaces(airspaces);
  csw->set_terrain(terrain);
  UpdateCrossSection();
  return csw;
}
示例#4
0
static void
Update()
{
  TCHAR sTmp[1000];

  assert(wf != NULL);
  assert(wInfo != NULL);
  assert(wGrid != NULL);
  assert(csw != NULL);
  assert(glide_computer != NULL);

  const ComputerSettings &settings_computer = blackboard->GetComputerSettings();
  const DerivedInfo &calculated = blackboard->Calculated();

  switch (page) {
  case AnalysisPage::BAROGRAPH:
    _stprintf(sTmp, _T("%s: %s"), _("Analysis"),
              _("Barograph"));
    wf->SetCaption(sTmp);
    BarographCaption(sTmp, glide_computer->GetFlightStats());
    wInfo->SetCaption(sTmp);
    SetCalcCaption(_("Settings"));
    break;

  case AnalysisPage::CLIMB:
    _stprintf(sTmp, _T("%s: %s"), _("Analysis"),
              _("Climb"));
    wf->SetCaption(sTmp);
    ClimbChartCaption(sTmp, glide_computer->GetFlightStats());
    wInfo->SetCaption(sTmp);
    SetCalcCaption(_("Task Calc"));
    break;

  case AnalysisPage::THERMAL_BAND:
    _stprintf(sTmp, _T("%s: %s"), _("Analysis"),
              _("Thermal Band"));
    wf->SetCaption(sTmp);
    ClimbChartCaption(sTmp, glide_computer->GetFlightStats());
    wInfo->SetCaption(sTmp);
    SetCalcCaption(_T(""));
    break;

  case AnalysisPage::WIND:
    _stprintf(sTmp, _T("%s: %s"), _("Analysis"),
              _("Wind at Altitude"));
    wf->SetCaption(sTmp);
    wInfo->SetCaption(_T(""));
    SetCalcCaption(_("Set Wind"));
    break;

  case AnalysisPage::POLAR:
    _stprintf(sTmp, _T("%s: %s (%s %d kg)"), _("Analysis"),
              _("Glide Polar"), _("Mass"),
              (int)settings_computer.polar.glide_polar_task.GetTotalMass());
    wf->SetCaption(sTmp);
    GlidePolarCaption(sTmp, settings_computer.polar.glide_polar_task);
    wInfo->SetCaption(sTmp);
    SetCalcCaption(_("Settings"));
   break;

  case AnalysisPage::TEMPTRACE:
    _stprintf(sTmp, _T("%s: %s"), _("Analysis"),
              _("Temp Trace"));
    wf->SetCaption(sTmp);
    TemperatureChartCaption(sTmp, glide_computer->GetCuSonde());
    wInfo->SetCaption(sTmp);
    SetCalcCaption(_("Settings"));
    break;

  case AnalysisPage::TASK_SPEED:
    _stprintf(sTmp, _T("%s: %s"), _("Analysis"),
              _("Task Speed"));
    wf->SetCaption(sTmp);
    wInfo->SetCaption(_T(""));
    SetCalcCaption(_("Task Calc"));
    break;

  case AnalysisPage::TASK:
    _stprintf(sTmp, _T("%s: %s"), _("Analysis"),
              _("Task"));
    wf->SetCaption(sTmp);
    FlightStatisticsRenderer::CaptionTask(sTmp, calculated);
    wInfo->SetCaption(sTmp);
    SetCalcCaption(_("Task calc"));
    break;

  case AnalysisPage::OLC:
    _stprintf(sTmp, _T("%s: %s"), _("Analysis"),
              ContestToString(settings_computer.contest.contest));
    wf->SetCaption(sTmp);
    SetCalcCaption(_T(""));
    FlightStatisticsRenderer::CaptionOLC(sTmp, settings_computer.contest,
                                         calculated);
    wInfo->SetCaption(sTmp);
    break;

  case AnalysisPage::AIRSPACE:
    _stprintf(sTmp, _T("%s: %s"), _("Analysis"),
              _("Airspace"));
    wf->SetCaption(sTmp);
    wInfo->SetCaption(_T(""));
    SetCalcCaption(_("Warnings"));
    break;

  case AnalysisPage::COUNT:
    gcc_unreachable();
  }

  switch (page) {
  case AnalysisPage::AIRSPACE:
    UpdateCrossSection();
    csw->Invalidate();
    csw->Show();
    wGrid->Hide();
    break;

  default:
    csw->Hide();
    wGrid->Show();
    wGrid->Invalidate();
    break;
  }
}
示例#5
0
static void
Update(void)
{
  TCHAR sTmp[1000];

  assert(wf != NULL);
  assert(wInfo != NULL);
  assert(wGrid != NULL);
  assert(csw != NULL);
  assert(glide_computer != NULL);

  const ComputerSettings &settings_computer = blackboard->GetComputerSettings();
  const DerivedInfo &calculated = blackboard->Calculated();

  FlightStatisticsRenderer fs(glide_computer->GetFlightStats(),
                              look->chart, look->map);

  switch (page) {
  case ANALYSIS_PAGE_BAROGRAPH:
    _stprintf(sTmp, _T("%s: %s"), _("Analysis"),
              _("Barograph"));
    wf->SetCaption(sTmp);
    fs.CaptionBarograph(sTmp);
    wInfo->SetCaption(sTmp);
    SetCalcCaption(_("Settings"));
    break;

  case ANALYSIS_PAGE_CLIMB:
    _stprintf(sTmp, _T("%s: %s"), _("Analysis"),
              _("Climb"));
    wf->SetCaption(sTmp);
    fs.CaptionClimb(sTmp);
    wInfo->SetCaption(sTmp);
    SetCalcCaption(_("Task Calc"));
    break;

  case ANALYSIS_PAGE_THERMAL_BAND:
    _stprintf(sTmp, _T("%s: %s"), _("Analysis"),
              _("Thermal Band"));
    wf->SetCaption(sTmp);
    fs.CaptionClimb(sTmp);
    wInfo->SetCaption(sTmp);
    SetCalcCaption(_T(""));
    break;

  case ANALYSIS_PAGE_WIND:
    _stprintf(sTmp, _T("%s: %s"), _("Analysis"),
              _("Wind At Altitude"));
    wf->SetCaption(sTmp);
    wInfo->SetCaption(_T(""));
    SetCalcCaption(_("Set Wind"));
    break;

  case ANALYSIS_PAGE_POLAR:
    _stprintf(sTmp, _T("%s: %s (%s %d kg)"), _("Analysis"),
              _("Glide Polar"), _("Mass"),
              (int)settings_computer.glide_polar_task.GetTotalMass());
    wf->SetCaption(sTmp);
    fs.CaptionPolar(sTmp, settings_computer.glide_polar_task);
    wInfo->SetCaption(sTmp);
    SetCalcCaption(_("Settings"));
   break;

  case ANALYSIS_PAGE_TEMPTRACE:
    _stprintf(sTmp, _T("%s: %s"), _("Analysis"),
              _("Temp Trace"));
    wf->SetCaption(sTmp);
    fs.CaptionTempTrace(sTmp, glide_computer->GetCuSonde());
    wInfo->SetCaption(sTmp);
    SetCalcCaption(_("Settings"));
    break;

  case ANALYSIS_PAGE_TASK_SPEED:
    _stprintf(sTmp, _T("%s: %s"), _("Analysis"),
              _("Task Speed"));
    wf->SetCaption(sTmp);
    wInfo->SetCaption(_T(""));
    SetCalcCaption(_("Task Calc"));
    break;

  case ANALYSIS_PAGE_TASK:
    _stprintf(sTmp, _T("%s: %s"), _("Analysis"),
              _("Task"));
    wf->SetCaption(sTmp);
    fs.CaptionTask(sTmp, calculated);
    wInfo->SetCaption(sTmp);
    SetCalcCaption(_("Task calc"));
    break;

  case ANALYSIS_PAGE_OLC:
    _stprintf(sTmp, _T("%s: %s"), _("Analysis"),
              ContestToString(settings_computer.task.contest));
    wf->SetCaption(sTmp);
    SetCalcCaption(_T(""));
    fs.CaptionOLC(sTmp, settings_computer.task, calculated);
    wInfo->SetCaption(sTmp);
    break;

  case ANALYSIS_PAGE_AIRSPACE:
    _stprintf(sTmp, _T("%s: %s"), _("Analysis"),
              _("Airspace"));
    wf->SetCaption(sTmp);
    wInfo->SetCaption(_T(""));
    SetCalcCaption(_("Warnings"));
    break;

  case ANALYSIS_PAGE_COUNT:
    assert(false);
    break;
  }

  switch (page) {
  case ANALYSIS_PAGE_AIRSPACE:
    UpdateCrossSection();
    csw->invalidate();
    csw->show();
    wGrid->hide();
    break;

  default:
    csw->hide();
    wGrid->show();
    wGrid->invalidate();
    break;
  }
}