SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized Class Reference

Inheritance diagram for SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized:

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_start
	altitude_end
	air_speed_start
	air_speed_end
	objective
	minimize
	lift_coefficient_limit
	seed_climb_rate
	algorithm
	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

Optimize your climb segment. This is useful if you're not sure how your vehicle should climb.
    You can set any conditions parameter as the objective, for example setting time to climb or vehicle mass:
    segment.objective       = 'conditions.weights.total_mass[-1,0]'
    
    The ending airspeed is an optional parameter.
    
    This segment takes far longer to run than a normal segment. Wrapping this into a vehicle optimization
    has not yet been tested for robustness.
    

    Assumptions:
    Can use SNOPT if you have it installed through PyOpt. But defaults to SLSQP through 
    Runs a linear true airspeed mission first to initialize conditions.
    
    Source:
    None

Member Function Documentation

__defaults__()

def SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized.__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.

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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/Climb/Optimized.py