Aero.FixedWing.criteriaTable

Class: Aero.FixedWing
Namespace: Aero

Construct criteria table for fixed-wing static stability analysis

Since R2021a

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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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`criteriatable` — Criteria table
6-by-N table

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

	U	V	W	Alpha	Beta	P	Q	R
FX	`"<"`	`''`	`''`	`''`	`''`	`''`	`''`	`''`
FY	`''`	`'<'`	`''`	`''`	`''`	`''`	`''`	`''`
FZ	`''`	`''`	`'<'`	`''`	`''`	`''`	`''`	`''`
L	`''`	`''`	`''`	`''`	`''`	`'<'`	`'<'`	`''`
M	`'>'`	`''`	`''`	`'<'`	`''`	`''`	`'<'`	`''`
N	`''`	`''`	`''`	`''`	`'>'`	`''`	`''`	`'<'`

Examples

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Calculate Static Stability of Cessna C182

Open Live Script

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