Public Member Functions | |
| def | __defaults__ (self) |
Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment | |
| def | initialize (self) |
| def | converge (self, state) |
| def | iterate (self) |
| def | finalize (self) |
| def | evaluate (self, state=None) |
| def | merged (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 | |
| altitude_start | |
| altitude_end | |
| descent_rate | |
| true_course | |
Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover | |
| altitude | |
| time | |
| true_course | |
Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic | |
| temperature_deviation | |
Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment | |
| settings | |
| state | |
| analyses | |
| process | |
| conditions | |
Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis | |
| tag | |
| features | |
| settings | |
A vertically descending hover for VTOL aircraft. Although the vehicle moves, no aerodynamic drag and lift are used.
Assumptions:
Your vehicle creates a negligible drag and lift force during a vertical descent.
Source:
None
| def SUAVE.Analyses.Mission.Segments.Hover.Descent.Descent.__defaults__ | ( | self | ) |
This sets the default solver flow. Anything in here can be modified after initializing a segment.
Assumptions:
None
Source:
N/A
Inputs:
None
Outputs:
None
Properties Used:
None
Reimplemented from SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover.