Mathematical Problems in Engineering / 2015 / Article / Tab 1

Research Article

Continuous Recursive Sliding Mode Control for Hypersonic Flight Vehicle with Extended Disturbance Observer

Table 1

Some parameters about simulation.

ParameterNotationValueUnit

Mass9375Slug
Moment of inertiaSlug⋅ft3
Reference area3603ft2
Mean aerodynamic chord80ft
Elevator coefficient0.0292Dimensionless
Density of airSlug/ft3

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