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;
}
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;
}
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;
}
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;
}
}
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;
}
}