本文整理汇总了Python中SUAVE.Core.Data.range方法的典型用法代码示例。如果您正苦于以下问题：Python Data.range方法的具体用法？Python Data.range怎么用？Python Data.range使用的例子？那么, 这里精选的方法代码示例或许可以为您提供帮助。您也可以进一步了解该方法所在类SUAVE.Core.Data的用法示例。
在下文中一共展示了Data.range方法的4个代码示例，这些例子默认根据受欢迎程度排序。您可以为喜欢或者感觉有用的代码点赞，您的评价将有助于系统推荐出更棒的Python代码示例。
示例1: short_field
# 需要导入模块: from SUAVE.Core import Data [as 别名]
# 或者: from SUAVE.Core.Data import range [as 别名]
def short_field(interface):
# unpack data
results_field = interface.results.takeoff_field_length
results_fuel = interface.results.fuel_for_missions
available_tofl = interface.analyses.missions.short_field.mission.airport.available_tofl
tofl_vec = results_field.takeoff_field_length
weight_vec_tofl = results_field.takeoff_weights
range_vec = results_fuel.distances
weight_vec_fuel = results_fuel.weights
fuel_vec = results_fuel.fuels
# evaluate maximum allowable takeoff weight from a given airfield
tow_short_field = np.interp(available_tofl,tofl_vec,weight_vec_tofl)
# determine maximum range/fuel based in tow short_field
range_short_field = np.interp(tow_short_field,weight_vec_fuel,range_vec)
fuel_short_field = np.interp(tow_short_field,weight_vec_fuel,fuel_vec)
# pack
results = Data()
results.tag = 'short_field'
results.takeoff_weight = tow_short_field
results.range = range_short_field
results.fuel = fuel_short_field
return results示例2: evaluate_range_from_short_field
# 需要导入模块: from SUAVE.Core import Data [as 别名]
# 或者: from SUAVE.Core.Data import range [as 别名]
def evaluate_range_from_short_field(vehicle,mission,results):
# unpack
airport_short_field = mission.airport_short_field
tofl = airport_short_field.field_lenght
takeoff_config = vehicle.configs.takeoff
from SUAVE.Methods.Performance import find_takeoff_weight_given_tofl
# evaluate maximum allowable takeoff weight from a short field
tow_short_field = find_takeoff_weight_given_tofl(vehicle,takeoff_config,airport_short_field,tofl)
# determine maximum range based in tow short_field
from SUAVE.Methods.Performance import size_mission_range_given_weights
# unpack
cruise_segment_tag = 'Cruise'
mission_payload = vehicle.mass_properties.payload
# call function
distance,fuel = size_mission_range_given_weights(vehicle,mission,cruise_segment_tag,mission_payload,tow_short_field)
# pack
short_field = Data()
short_field.tag = 'short_field'
short_field.takeoff_weight = tow_short_field
short_field.range = distance
short_field.fuel = fuel
results.short_field = short_field
return results示例3: mission_fuel
# 需要导入模块: from SUAVE.Core import Data [as 别名]
# 或者: from SUAVE.Core.Data import range [as 别名]
def mission_fuel(interface):
# unpack data
design_range = interface.analyses.missions.fuel.range
range_vec = interface.results.fuel_for_missions.distances
fuel_vec = interface.results.fuel_for_missions.fuels
# determine maximum range/fuel based in tow short_field
fuel_design_mission = np.interp(design_range,range_vec,fuel_vec)
# pack results
results = Data()
results.tag = 'design_mission'
results.range = design_range
results.fuel = fuel_design_mission
return results示例4: max_range
# 需要导入模块: from SUAVE.Core import Data [as 别名]
# 或者: from SUAVE.Core.Data import range [as 别名]
def max_range(interface):
# unpack data
max_takeoff_weight = interface.configs.base.mass_properties.max_takeoff
range_vec = interface.results.fuel_for_missions.distances
weight_vec_fuel = interface.results.fuel_for_missions.weights
fuel_vec = interface.results.fuel_for_missions.fuels
# determine maximum range/fuel based in max_tow
range = np.interp(max_takeoff_weight,weight_vec_fuel,range_vec)
fuel = np.interp(max_takeoff_weight,weight_vec_fuel,fuel_vec)
# pack results
results = Data()
results.tag = 'short_field'
results.takeoff_weight = max_takeoff_weight
results.range = range
results.fuel = fuel
return results