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