SUAVE  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
SUAVE.Components.Configs.Config.Config Class Reference
Inheritance diagram for SUAVE.Components.Configs.Config.Config:
SUAVE.Vehicle.Vehicle SUAVE.Core.Data.Data

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Vehicle.Vehicle
def __init__ (self, *args, **kwarg)
 
def find_component_root (self, component)
 
def append_component (self, component)
 
def sum_mass (self)
 
def center_of_gravity (self)
 
- Public Member Functions inherited from SUAVE.Core.Data.Data
def __getattribute__ (self, k)
 
def __setattr__ (self, k, v)
 
def __delattr__ (self, k)
 
def __new__ (cls, *args, **kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __iter__ (self)
 
def itervalues (self)
 
def values (self)
 
def update (self, other)
 
def append_or_update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
 
def deep_set (self, keys, val)
 
def deep_get (self, keys)
 
def pack_array (self, output='vector')
 
def unpack_array (self, M)
 
def do_recursive (self, method, other=None, default=None)
 

Public Attributes

 tag
 
- Public Attributes inherited from SUAVE.Vehicle.Vehicle
 tag
 
 fuselages
 
 wings
 
 networks
 
 nacelles
 
 systems
 
 mass_properties
 
 payload
 
 costs
 
 envelope
 
 landing_gear
 
 reference_area
 
 passengers
 
 performance
 

Detailed Description

SUAVE.Components.Config()

    The Top Level Configuration Class
    
        Assumptions:
        None
        
        Source:
        N/A

Member Function Documentation

◆ __defaults__()

def SUAVE.Components.Configs.Config.Config.__defaults__ (   self)
This sets the default values for the configuration.

Assumptions:
None

Source:
N/A

Inputs:
None

Outputs:
None

Properties Used:
N/A

Reimplemented from SUAVE.Vehicle.Vehicle.


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