Aero.FixedWing.criteriaTable

Class: Aero.FixedWing
Namespace: Aero

Construct criteria table for fixed-wing static stability analysis

Since R2021a

Syntax

criteriatable = Aero.FixedWing.criteriaTable()


Description

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

Output Arguments

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

Calculate Static Stability of Cessna C182

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