bool
AbstractTask::UpdateIdle(const AircraftState &state,
const GlidePolar &glide_polar)
{
if (TaskStarted() && task_behaviour.calc_cruise_efficiency) {
fixed val = fixed_one;
if (CalcCruiseEfficiency(state, glide_polar, val))
stats.cruise_efficiency = std::max(ce_lpf.update(val), fixed_zero);
} else {
stats.cruise_efficiency = ce_lpf.reset(fixed_one);
}
if (TaskStarted() && task_behaviour.calc_effective_mc) {
fixed val = glide_polar.GetMC();
if (CalcEffectiveMC(state, glide_polar, val))
stats.effective_mc = std::max(em_lpf.update(val), fixed_zero);
} else {
stats.effective_mc = em_lpf.reset(glide_polar.GetMC());
}
if (task_behaviour.calc_glide_required)
UpdateStatsGlide(state, glide_polar);
else
stats.glide_required = fixed_zero; // error
return false;
}
bool
AbstractTask::UpdateIdle(const AircraftState &state,
const GlidePolar &glide_polar)
{
if (stats.start.task_started && task_behaviour.calc_cruise_efficiency &&
glide_polar.IsValid()) {
fixed val = fixed(1);
if (CalcCruiseEfficiency(state, glide_polar, val))
stats.cruise_efficiency = std::max(ce_lpf.Update(val), fixed(0));
} else {
stats.cruise_efficiency = ce_lpf.Reset(fixed(1));
}
if (stats.start.task_started && task_behaviour.calc_effective_mc &&
glide_polar.IsValid()) {
fixed val = glide_polar.GetMC();
if (CalcEffectiveMC(state, glide_polar, val))
stats.effective_mc = std::max(em_lpf.Update(val), fixed(0));
} else {
stats.effective_mc = em_lpf.Reset(glide_polar.GetMC());
}
if (task_behaviour.calc_glide_required && glide_polar.IsValid())
UpdateStatsGlide(state, glide_polar);
else
stats.glide_required = fixed(0); // error
return false;
}
