def test_list_parameters(self):
params = list_parameters()
self.assertIn('Airspeed', params) # LFL
self.assertIn('Altitude AAL', params) # Derived Node
# ensure dependencies of other modules (not in derived) are included
self.assertIn('TAWS General', params)
self.assertIn('Key Satcom (1)', params)
# ensure KPV and KTIs are excluded
self.assertNotIn('AOA With Flap 15 Max', params) # KPV
self.assertNotIn('Landing Turn Off Runway', params) # KTI
self.assertNotIn('FDR Takeoff Runway', params) # Attribute
# other non base 2 frequencies
0.016666667,
0.05,
0.1,
0.2,
5,
10,
20,
}
# -----------------------------------------------------------------------------
# Collection of parameters known to Polaris
# -----------------------------------------------------------------------------
# Main list of parameters that from the Polaris analysis engine
PARAMETERS_ANALYSIS = list_parameters()
# Minimum list of parameters (including alternatives) needed in the HDF file.
# See check_for_core_parameters method
PARAMETERS_CORE = [
u'Airspeed',
u'Heading',
u'Altitude STD',
# Helicopter only
u'Nr',
# Alternatives
u'Heading True',
u'Nr (1)',
u'Nr (2)',
]
# other non base 2 frequencies
0.016666667,
0.05,
0.1,
0.2,
5,
10,
20,
}
# -----------------------------------------------------------------------------
# Collection of parameters known to Polaris
# -----------------------------------------------------------------------------
# Main list of parameters that from the Polaris analysis engine
PARAMETERS_ANALYSIS = list_parameters()
# Minimum list of parameters (including alternatives) needed in the HDF file.
# See check_for_core_parameters method
PARAMETERS_CORE = [
u'Airspeed',
u'Heading',
u'Altitude STD',
# Helicopter only
u'Nr',
# Alternatives
u'Heading True',
u'Nr (1)',
u'Nr (2)',
]
