def circling_left(flight, **kwargs):
return FlightPhase(
flight=flight,
aggregate=True,
phase_type=FlightPhase.PT_CIRCLING,
circling_direction=FlightPhase.CD_LEFT,
alt_diff=5335.0,
duration=timedelta(seconds=3776),
fraction=26.0,
vario=1.41313559322034,
count=17,
).apply_kwargs(kwargs)
def circling_mixed(flight, **kwargs):
return FlightPhase(
flight=flight,
aggregate=True,
phase_type=FlightPhase.PT_CIRCLING,
circling_direction=FlightPhase.CD_MIXED,
alt_diff=2863.0,
duration=timedelta(seconds=2796),
fraction=19.0,
vario=1.02396280400573,
count=7,
).apply_kwargs(kwargs)
def circling_right(flight, **kwargs):
return FlightPhase(
flight=flight,
aggregate=True,
phase_type=FlightPhase.PT_CIRCLING,
circling_direction=FlightPhase.CD_RIGHT,
alt_diff=11344.0,
duration=timedelta(seconds=7900),
fraction=55.0,
vario=1.43607594936709,
count=54,
).apply_kwargs(kwargs)
def circling(flight, **kwargs):
return FlightPhase(
flight=flight,
aggregate=True,
phase_type=FlightPhase.PT_CIRCLING,
circling_direction=FlightPhase.CD_TOTAL,
alt_diff=19543.0,
duration=timedelta(seconds=14472),
fraction=37.0,
vario=1.35046987285793,
count=78,
).apply_kwargs(kwargs)
def cruise(flight, **kwargs):
return FlightPhase(
flight=flight,
aggregate=True,
phase_type=FlightPhase.PT_CRUISE,
alt_diff=-20647.0,
duration=timedelta(seconds=24312),
fraction=63.0,
distance=837677.0,
speed=34.4552944491395,
vario=-0.849292530437643,
glide_rate=40.5694071410054,
count=79,
).apply_kwargs(kwargs)
def example2(flight, **kwargs):
return FlightPhase(
flight=flight,
start_time=datetime(2016, 5, 4, 17, 59, 6),
end_time=datetime(2016, 5, 4, 17, 59, 6) + timedelta(seconds=44),
aggregate=False,
phase_type=FlightPhase.PT_CRUISE,
alt_diff=-93.0,
duration=timedelta(seconds=44),
distance=977.0,
speed=22.2232648999519,
vario=-2.11363636363637,
glide_rate=10.5142328558912,
count=1,
).apply_kwargs(kwargs)
def example1(flight, **kwargs):
return FlightPhase(
flight=flight,
start_time=datetime(2016, 5, 4, 17, 54, 6),
end_time=datetime(2016, 5, 4, 17, 54, 6) + timedelta(seconds=300),
aggregate=False,
phase_type=FlightPhase.PT_CIRCLING,
circling_direction=FlightPhase.CD_RIGHT,
alt_diff=417.0,
duration=timedelta(seconds=300),
distance=7028.0,
speed=23.4293014168156,
vario=1.39000000000002,
glide_rate=-16.8556125300829,
count=1,
).apply_kwargs(kwargs)
def save_phases(root, flight):
if 'phases' not in root or 'performance' not in root:
return
phases = []
PT_IDX = {'powered': FlightPhase.PT_POWERED,
'cruise': FlightPhase.PT_CRUISE,
'circling': FlightPhase.PT_CIRCLING}
CD_IDX = {'': None,
'left': FlightPhase.CD_LEFT,
'mixed': FlightPhase.CD_MIXED,
'right': FlightPhase.CD_RIGHT,
'total': FlightPhase.CD_TOTAL}
for phdata in root['phases']:
ph = FlightPhase()
ph.flight = flight
ph.aggregate = False
ph.start_time = import_datetime_attribute(phdata, 'start_time')
ph.end_time = import_datetime_attribute(phdata, 'end_time')
ph.phase_type = PT_IDX[phdata['type']]
ph.circling_direction = CD_IDX[phdata['circling_direction']]
ph.alt_diff = phdata['alt_diff']
ph.duration = datetime.timedelta(seconds=phdata['duration'])
ph.distance = phdata['distance']
ph.speed = phdata['speed']
ph.vario = phdata['vario']
ph.glide_rate = phdata['glide_rate']
ph.count = 1
phases.append(ph)
for statname in ["total", "left", "right", "mixed"]:
phdata = root['performance']["circling_%s" % statname]
ph = FlightPhase()
ph.aggregate = True
ph.phase_type = FlightPhase.PT_CIRCLING
ph.fraction = round(phdata['fraction'] * 100)
ph.circling_direction = CD_IDX[statname]
ph.alt_diff = phdata['alt_diff']
ph.duration = datetime.timedelta(seconds=phdata['duration'])
ph.vario = phdata['vario']
ph.count = phdata['count']
phases.append(ph)
phdata = root['performance']['cruise_total']
ph = FlightPhase()
ph.aggregate = True
ph.phase_type = FlightPhase.PT_CRUISE
ph.circling_direction = FlightPhase.CD_TOTAL
ph.alt_diff = phdata['alt_diff']
ph.duration = datetime.timedelta(seconds=phdata['duration'])
ph.fraction = round(phdata['fraction'] * 100)
ph.distance = phdata['distance']
ph.speed = phdata['speed']
ph.vario = phdata['vario']
ph.glide_rate = phdata['glide_rate']
ph.count = phdata['count']
phases.append(ph)
flight._phases = phases
def save_phases(root, flight):
flight.delete_phases()
if 'phases' not in root or 'performance' not in root:
return
PT_IDX = {'': None,
'powered': FlightPhase.PT_POWERED,
'cruise': FlightPhase.PT_CRUISE,
'circling': FlightPhase.PT_CIRCLING}
CD_IDX = {'': None,
'left': FlightPhase.CD_LEFT,
'mixed': FlightPhase.CD_MIXED,
'right': FlightPhase.CD_RIGHT,
'total': FlightPhase.CD_TOTAL}
for phdata in root['phases']:
ph = FlightPhase()
ph.aggregate = False
ph.start_time = import_datetime_attribute(phdata, 'start_time')
ph.end_time = import_datetime_attribute(phdata, 'end_time')
ph.phase_type = PT_IDX[phdata['type']]
ph.circling_direction = CD_IDX[phdata['circling_direction']]
ph.alt_diff = phdata['alt_diff']
ph.duration = datetime.timedelta(seconds=phdata['duration'])
ph.distance = phdata['distance']
ph.speed = phdata['speed']
ph.vario = phdata['vario']
ph.glide_rate = phdata['glide_rate']
ph.count = 1
flight._phases.append(ph)
for statname in ["total", "left", "right", "mixed"]:
phdata = root['performance']["circling_%s" % statname]
ph = FlightPhase()
ph.aggregate = True
ph.phase_type = FlightPhase.PT_CIRCLING
ph.fraction = round(phdata['fraction'] * 100)
ph.circling_direction = CD_IDX[statname]
ph.alt_diff = phdata['alt_diff']
ph.duration = datetime.timedelta(seconds=phdata['duration'])
ph.vario = phdata['vario']
ph.count = phdata['count']
flight._phases.append(ph)
phdata = root['performance']['cruise_total']
ph = FlightPhase()
ph.aggregate = True
ph.phase_type = FlightPhase.PT_CRUISE
ph.circling_direction = FlightPhase.CD_TOTAL
ph.alt_diff = phdata['alt_diff']
ph.duration = datetime.timedelta(seconds=phdata['duration'])
ph.fraction = round(phdata['fraction'] * 100)
ph.distance = phdata['distance']
ph.speed = phdata['speed']
ph.vario = phdata['vario']
ph.glide_rate = phdata['glide_rate']
ph.count = phdata['count']
flight._phases.append(ph)
def save_phases(root, flight):
flight.delete_phases()
if "phases" not in root or "performance" not in root:
return
PT_IDX = {
"": None,
"powered": FlightPhase.PT_POWERED,
"cruise": FlightPhase.PT_CRUISE,
"circling": FlightPhase.PT_CIRCLING,
}
CD_IDX = {
"": None,
"left": FlightPhase.CD_LEFT,
"mixed": FlightPhase.CD_MIXED,
"right": FlightPhase.CD_RIGHT,
"total": FlightPhase.CD_TOTAL,
}
for phdata in root["phases"]:
ph = FlightPhase()
ph.aggregate = False
ph.start_time = import_datetime_attribute(phdata, "start_time")
ph.end_time = import_datetime_attribute(phdata, "end_time")
ph.phase_type = PT_IDX[phdata["type"]]
ph.circling_direction = CD_IDX[phdata["circling_direction"]]
ph.alt_diff = phdata["alt_diff"]
ph.duration = datetime.timedelta(seconds=phdata["duration"])
ph.distance = phdata["distance"]
ph.speed = phdata["speed"]
ph.vario = phdata["vario"]
ph.glide_rate = phdata["glide_rate"]
ph.count = 1
flight._phases.append(ph)
for statname in ["total", "left", "right", "mixed"]:
phdata = root["performance"]["circling_%s" % statname]
ph = FlightPhase()
ph.aggregate = True
ph.phase_type = FlightPhase.PT_CIRCLING
ph.fraction = round(phdata["fraction"] * 100)
ph.circling_direction = CD_IDX[statname]
ph.alt_diff = phdata["alt_diff"]
ph.duration = datetime.timedelta(seconds=phdata["duration"])
ph.vario = phdata["vario"]
ph.count = phdata["count"]
flight._phases.append(ph)
phdata = root["performance"]["cruise_total"]
ph = FlightPhase()
ph.aggregate = True
ph.phase_type = FlightPhase.PT_CRUISE
ph.circling_direction = FlightPhase.CD_TOTAL
ph.alt_diff = phdata["alt_diff"]
ph.duration = datetime.timedelta(seconds=phdata["duration"])
ph.fraction = round(phdata["fraction"] * 100)
ph.distance = phdata["distance"]
ph.speed = phdata["speed"]
ph.vario = phdata["vario"]
ph.glide_rate = phdata["glide_rate"]
ph.count = phdata["count"]
flight._phases.append(ph)
def save_phases(root, flight):
flight.delete_phases()
if "phases" not in root or "performance" not in root:
return
PT_IDX = {
"": None,
"powered": FlightPhase.PT_POWERED,
"cruise": FlightPhase.PT_CRUISE,
"circling": FlightPhase.PT_CIRCLING,
}
CD_IDX = {
"": None,
"left": FlightPhase.CD_LEFT,
"mixed": FlightPhase.CD_MIXED,
"right": FlightPhase.CD_RIGHT,
"total": FlightPhase.CD_TOTAL,
}
for phdata in root["phases"]:
ph = FlightPhase()
ph.aggregate = False
ph.start_time = import_datetime_attribute(phdata, "start_time")
ph.end_time = import_datetime_attribute(phdata, "end_time")
ph.phase_type = PT_IDX[phdata["type"]]
ph.circling_direction = CD_IDX[phdata["circling_direction"]]
ph.alt_diff = phdata["alt_diff"]
ph.duration = datetime.timedelta(seconds=phdata["duration"])
ph.distance = phdata["distance"]
ph.speed = phdata["speed"]
ph.vario = phdata["vario"]
ph.glide_rate = phdata["glide_rate"]
ph.count = 1
flight._phases.append(ph)
for statname in ["total", "left", "right", "mixed"]:
phdata = root["performance"]["circling_%s" % statname]
ph = FlightPhase()
ph.aggregate = True
ph.phase_type = FlightPhase.PT_CIRCLING
ph.fraction = round(phdata["fraction"] * 100)
ph.circling_direction = CD_IDX[statname]
ph.alt_diff = phdata["alt_diff"]
ph.duration = datetime.timedelta(seconds=phdata["duration"])
ph.vario = phdata["vario"]
ph.count = phdata["count"]
flight._phases.append(ph)
phdata = root["performance"]["cruise_total"]
ph = FlightPhase()
ph.aggregate = True
ph.phase_type = FlightPhase.PT_CRUISE
ph.circling_direction = FlightPhase.CD_TOTAL
ph.alt_diff = phdata["alt_diff"]
ph.duration = datetime.timedelta(seconds=phdata["duration"])
ph.fraction = round(phdata["fraction"] * 100)
ph.distance = phdata["distance"]
ph.speed = phdata["speed"]
ph.vario = phdata["vario"]
ph.glide_rate = phdata["glide_rate"]
ph.count = phdata["count"]
flight._phases.append(ph)