SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude Class Reference

Inheritance diagram for SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude:

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
	altitude
	air_speed
	distance
	true_course
Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
	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 CLASSIC! Fixed true airspeed and altitude and a set distance.
    Most other cruise segments are built off this segment. The most simple segment you can fly.

    Assumptions:
    None
    
    Source:
    None

Member Function Documentation

__defaults__()

def SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude.__defaults__

(

self

)

This sets the default solver flow. Anything in here can be modified after initializing a segment.
    
    Assumptions:
    None
    
    Source:
    N/A
    
    Inputs:
    None
    
    Outputs:
    None
    
    Properties Used:
    None

Reimplemented from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic.

Reimplemented in 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.Cruise.Constant_Dynamic_Pressure_Constant_Altitude.Constant_Dynamic_Pressure_Constant_Altitude, and SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude.Constant_Mach_Constant_Altitude.

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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/Cruise/Constant_Speed_Constant_Altitude.py