SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic Class Reference

Inheritance diagram for SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic:

Public Member Functions
def	__defaults__ (self)
Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def	initialize (self)
def	converge (self, state)
def	iterate (self)
def	finalize (self)
def	evaluate (self, state=None)
def	merged (self)
Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def	compile (self, *args, **kwarg)
def	initialize (self, *args, **kwarg)
def	evaluate (self, *args, **kwarg)
def	finalize (self, *args, **kwarg)
def	__call__ (self, *args, **kwarg)

Public Attributes
	temperature_deviation
Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
	settings
	state
	analyses
	process
	conditions
Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
	tag
	features
	settings

Detailed Description

The third basic piece of a mission which each segment will expand upon

    Assumptions:
    There's a detailed process flow outline in defaults. A mission must be solved in that order.
    Assumes you're an atmospheric vehicle.
    
    Source:
    None

Member Function Documentation

__defaults__()

def SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic.__defaults__

(

self

)

This sets the default values.
    
    Assumptions:
    None
    
    Source:
    N/A
    
    Inputs:
    None
    
    Outputs:
    None
    
    Properties Used:
    None

Reimplemented from SUAVE.Analyses.Mission.Segments.Simple.Simple.

Reimplemented in SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground, SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized, SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing, SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff, SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed, SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude, SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude, SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude_No_Propulsion.Set_Speed_Set_Altitude_No_Propulsion, SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude, SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude, SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle, SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude, SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise, SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb.Constant_Acceleration_Constant_Angle_Linear_Climb, SUAVE.Analyses.Mission.Segments.Hover.Climb.Climb, SUAVE.Analyses.Mission.Segments.Hover.Descent.Descent, SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover, SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise, SUAVE.Analyses.Mission.Segments.Climb.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate, SUAVE.Analyses.Mission.Segments.Climb.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate, SUAVE.Analyses.Mission.Segments.Descent.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate, SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate, SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.Constant_Dynamic_Pressure_Constant_Angle, SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Angle.Constant_Mach_Constant_Angle, SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Rate.Constant_Mach_Constant_Rate, SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle, SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate, SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.Constant_Dynamic_Pressure_Constant_Altitude_Loiter, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.Constant_Mach_Constant_Altitude_Loiter, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.Constant_Speed_Constant_Altitude_Loiter, SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle, SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Linear_Altitude.Constant_Mach_Linear_Altitude, SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude.Constant_Dynamic_Pressure_Constant_Altitude, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude.Constant_Mach_Constant_Altitude, SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.Constant_Dynamic_Pressure_Constant_Rate, SUAVE.Analyses.Mission.Segments.Ground.Battery_Charge_Discharge.Battery_Charge_Discharge, SUAVE.Analyses.Mission.Segments.Descent.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate, and SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate.

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The documentation for this class was generated from the following file:

• /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Aerodynamic.py