Public Member Functions | |
def | __defaults__ (self) |
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 | |
mass_properties | |
Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis | |
tag | |
features | |
settings | |
This is a class that call the functions that computes the weight of an aircraft depending on its configration Assumptions: None Source: N/A Inputs: None Outputs: None Properties Used: N/A
def SUAVE.Analyses.Weights.Weights.Weights.__defaults__ | ( | self | ) |
This sets the default values and methods for the weights analysis. Assumptions: None Source: N/A Inputs: None Outputs: None Properties Used: N/A
Reimplemented from SUAVE.Analyses.Analysis.Analysis.
Reimplemented in SUAVE.Analyses.Weights.Weights_eVTOL.Weights_eVTOL, SUAVE.Analyses.Weights.Weights_Transport.Weights_Transport, SUAVE.Analyses.Weights.Weights_BWB.Weights_BWB, and SUAVE.Analyses.Weights.Weights_UAV.Weights_UAV.
def SUAVE.Analyses.Weights.Weights.Weights.evaluate | ( | self, | |
conditions = None |
|||
) |
Evaluate the weight analysis. Assumptions: None Source: N/A Inputs: self.vehicle [Data] self.settings [Data] self.settings.empty [Data] Outputs: self.weight_breakdown [Data] results [Data] Properties Used: N/A
Reimplemented in SUAVE.Analyses.Weights.Weights_Transport.Weights_Transport.
def SUAVE.Analyses.Weights.Weights.Weights.finalize | ( | self | ) |
Finalize the weight analysis. Assumptions: None Source: N/A Inputs: None Outputs: None Properties Used: N/A