SUAVE  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
SUAVE.Analyses.Weights.Weights_UAV.Weights_UAV Class Reference
Inheritance diagram for SUAVE.Analyses.Weights.Weights_UAV.Weights_UAV:
SUAVE.Analyses.Weights.Weights.Weights SUAVE.Analyses.Analysis.Analysis

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Weights.Weights.Weights
def evaluate (self, conditions=None)
 
def finalize (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

 tag
 
 vehicle
 
 settings
 
- Public Attributes inherited from SUAVE.Analyses.Weights.Weights.Weights
 tag
 
 vehicle
 
 settings
 
 mass_properties
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
 
 features
 
 settings
 

Detailed Description

This is class that evaluates the weight of a UAV

Assumptions:
    None

Source:
    N/A

Inputs:
    None
  
Outputs:
    None

Properties Used:
    N/A

Member Function Documentation

◆ __defaults__()

def SUAVE.Analyses.Weights.Weights_UAV.Weights_UAV.__defaults__ (   self)
This sets the default values and methods for the UAV weight analysis.
    
Assumptions:
None

Source:
N/A

Inputs:
None

Outputs:
None

Properties Used:
N/A

Reimplemented from SUAVE.Analyses.Weights.Weights.Weights.


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