Public Member Functions | |
| def | __defaults__ (self) |
| def | finalize (self) |
| def | __call__ (self, conditions) |
| def | sample_training (self) |
| def | build_surrogate (self) |
| def | evaluate_conditions (self, run_conditions, trim_aircraft) |
Public Member Functions inherited from SUAVE.Analyses.Stability.Stability.Stability | |
| def | evaluate (self, conditions) |
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 | |
| current_status | |
| geometry | |
| settings | |
| training | |
| training_file | |
| surrogates | |
| configuration | |
Public Attributes inherited from SUAVE.Analyses.Stability.Stability.Stability | |
| tag | |
| geometry | |
| settings | |
Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis | |
| tag | |
| features | |
| settings | |
This builds a surrogate and computes moment using AVL. Assumptions: None Source: None
| def SUAVE.Analyses.Stability.AVL.AVL.__call__ | ( | self, | |
| conditions | |||
| ) |
Evaluates moment coefficient, stability and body axis deriviatives and neutral point using available surrogates.
Assumptions:
None
Source:
N/A
Inputs:
state.conditions.
mach_number [-]
angle_of_attack [radians]
Outputs:
results
results.stability.static
results.stability.dynamic
Properties Used:
self.surrogates.
pitch_moment_coefficient [-] CM
cm_alpha [-] Cm_alpha
cn_beta [-] Cn_beta
neutral_point [-] NP
| def SUAVE.Analyses.Stability.AVL.AVL.__defaults__ | ( | self | ) |
This sets the default values and methods for the analysis. Assumptions: None Source: N/A Inputs: None Outputs: None Properties Used: N/A
Reimplemented from SUAVE.Analyses.Stability.Stability.Stability.
| def SUAVE.Analyses.Stability.AVL.AVL.build_surrogate | ( | self | ) |
Builds a surrogate based on sample evalations using a Guassian process. Assumptions: None Source: N/A Inputs: self.training. coefficients [-] CM, Cm_alpha, Cn_beta neutral point [meters] NP grid_points [radians,-] angles of attack and Mach numbers Outputs: self.surrogates. moment_coefficient Cm_alpha_moment_coefficient Cn_beta_moment_coefficient neutral_point Properties Used: No others
| def SUAVE.Analyses.Stability.AVL.AVL.evaluate_conditions | ( | self, | |
| run_conditions, | |||
| trim_aircraft | |||
| ) |
Process vehicle to setup geometry, condititon, and configuration. Assumptions: None Source: N/A Inputs: run_conditions <SUAVE data type> aerodynamic conditions; until input method is finalized, will assume mass_properties are always as defined in self.features Outputs: results <SUAVE data type> Properties Used: self.settings.filenames. run_folder output_template batch_template deck_template self.current_status. batch_index batch_file deck_file cases
| def SUAVE.Analyses.Stability.AVL.AVL.finalize | ( | self | ) |
Drives functions to get training samples and build a surrogate.
Assumptions:
None
Source:
N/A
Inputs:
None
Outputs:
self.tag = 'avl_analysis_of_{}'.format( )
Properties Used:
self.geometry.tag
Reimplemented from SUAVE.Analyses.Stability.Stability.Stability.
| def SUAVE.Analyses.Stability.AVL.AVL.sample_training | ( | self | ) |
Call methods to run AVL for sample point evaluation. Assumptions: None Source: N/A Inputs: see properties used Outputs: self.training. coefficients [-] CM, Cm_alpha, Cn_beta neutral point [-] NP grid_points [radians,-] angles of attack and Mach numbers Properties Used: self.geometry.tag <string> self.training. angle_of_attack [radians] Mach [-] self.training_file (optional - file containing previous AVL data)