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Aero.FixedWing.criteriaTable

Class: Aero.FixedWing
Package: Aero

Construct criteria table for fixed-wing static stability analysis

Syntax

criteriatable = Aero.FixedWing.criteriaTable()

Description

criteriatable = Aero.FixedWing.criteriaTable() constructs a criteria table for fixed-wing static stability analysis.

Output Arguments

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Criteria table, returned as a 6-by-N table where N is number of variables. By default, this table appears as follows:

 UVWAlphaBetaPQR
FX"<"''''''''''''''
FY'''<'''''''''''''
FZ'''''<'''''''''''
L'''''''''''<''<'''
M'>''''''<''''''<'''
N'''''''''>''''''<'

Examples

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Calculate the static stability of a Cessna C182.

[C182, CruiseState] = astC182();
stability = staticStability(C182, CruiseState)
stability =

  6×8 table

             U           V           W         Alpha        Beta         P           Q           R    
          ________    ________    ________    ________    ________    ________    ________    ________

    FX    "Stable"    ""          ""          ""          ""          ""          ""          ""      
    FY    ""          "Stable"    ""          ""          ""          ""          ""          ""      
    FZ    ""          ""          "Stable"    ""          ""          ""          ""          ""      
    L     ""          ""          ""          ""          "Stable"    "Stable"    ""          ""      
    M     "Stable"    ""          ""          "Stable"    ""          ""          "Stable"    ""      
    N     ""          ""          ""          ""          "Stable"    ""          ""          "Stable"

Version History

Introduced in R2021a