added new phase info file

aviary/interface/default_phase_info/height_energy_fiti.py

@@ -0,0 +1,95 @@
+from aviary.mission.flops_based.phases.time_integration_phases import SGMDetailedTakeoff, \
+    SGMHeightEnergy, SGMDetailedLanding
+from aviary.subsystems.propulsion.propulsion_builder import CorePropulsionBuilder
+from aviary.subsystems.geometry.geometry_builder import CoreGeometryBuilder
+from aviary.subsystems.mass.mass_builder import CoreMassBuilder
+from aviary.subsystems.aerodynamics.aerodynamics_builder import CoreAerodynamicsBuilder
+from aviary.utils.aviary_values import AviaryValues
+from aviary.variable_info.variable_meta_data import _MetaData as BaseMetaData
+from aviary.variable_info.variables import Dynamic, Mission
+from aviary.variable_info.enums import SpeedType, Verbosity, AlphaModes, LegacyCode
+
+from aviary.interface.default_phase_info.two_dof_fiti_copy import add_default_sgm_args
+
+FLOPS = LegacyCode.FLOPS
+
+prop = CorePropulsionBuilder('core_propulsion', BaseMetaData)
+mass = CoreMassBuilder('core_mass', BaseMetaData, FLOPS)
+aero = CoreAerodynamicsBuilder('core_aerodynamics', BaseMetaData, FLOPS)
+geom = CoreGeometryBuilder('core_geometry', BaseMetaData, FLOPS)
+
+default_premission_subsystems = [prop, geom, mass, aero]
+default_mission_subsystems = [aero, prop]
+
+cruise_mach = .8,
+cruise_alt = 35e3,
+
+phase_info = {
+    "pre_mission": {"include_takeoff": False, "optimize_mass": True},
+    "climb": {
+        'builder': SGMHeightEnergy,
+        "user_options": {
+            'mach': (cruise_mach, 'unitless'),
+            'alt_trigger': (cruise_alt, 'ft'),
+        },
+    },
+    "cruise": {
+        'kwargs': dict(
+            input_speed_type=SpeedType.MACH,
+            input_speed_units="unitless",
+            alpha_mode=AlphaModes.REQUIRED_LIFT,
+        ),
+        'builder': SGMHeightEnergy,
+        "user_options": {
+            'mach': (cruise_mach, 'unitless'),
+        },
+    },
+    "descent": {
+        'builder': SGMHeightEnergy,
+        "user_options": {
+            'mach': (cruise_mach, 'unitless'),
+            'alt_trigger': (1000, 'ft'),
+            Dynamic.Mission.THROTTLE: (0, 'unitless'),
+        },
+    },
+    "post_mission": {
+        "include_landing": False,
+        "constrain_range": True,
+        "target_range": (1906., "nmi"),
+    },
+}
+
+
+def phase_info_parameterization(phase_info, post_mission_info, aviary_inputs: AviaryValues):
+    """
+    Modify the values in the phase_info dictionary to accomodate different values
+    for the following mission design inputs: cruise altitude, cruise mach number,
+    cruise range, design gross mass.
+
+    Parameters
+    ----------
+    phase_info : dict
+        Dictionary of phase settings for a mission profile
+    aviary_inputs : <AviaryValues>
+        Object containing values and units for all aviary inputs and options
+
+    Returns
+    -------
+    dict
+        Modified phase_info that has been changed to match the new mission
+        parameters
+    """
+
+    range_cruise = aviary_inputs.get_item(Mission.Design.RANGE)
+    alt_cruise = aviary_inputs.get_item(Mission.Design.CRUISE_ALTITUDE)
+    gross_mass = aviary_inputs.get_item(Mission.Design.GROSS_MASS)
+    mach_cruise = aviary_inputs.get_item(Mission.Design.MACH)
+
+    phase_info['climb']['user_options']['alt_trigger'] = alt_cruise
+    phase_info['climb']['user_options']['mach'] = mach_cruise
+
+    phase_info['cruise']['user_options']['mach'] = mach_cruise
+
+    phase_info['descent']['user_options']['mach'] = mach_cruise
+
+    return phase_info, post_mission_info