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Path: ACPro/Wind
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Wind gust model. Generates state space equations or spectral densities.
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Form:
g = WindGust( h, u0, sigma, wingSpan, f, w )
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Inputs
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h (:,:) Altitude (m)
u0 (1,1) Aircraft mean speed wrt air mass
sigma (3,1) Standard deviation of the gust velocity
sigma.u
sigma.v
sigma.w
wingSpan (1,1) Wing span
f function to be performed
'spectral' spectral densities
'state' state space equations for velocity
'accel' state space equations for acceleration
w (1,:) Frequencies at which to compute power spectral densities
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Outputs
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g Wind gust output of type statespace
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Reference: McRuer, D., Ashkenas, I., and D. Graham, Aircraft Dynamics
and Automatic Control," Princeton, 1973, p 654.
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Common: Classes/@statespace/and.m Common: Classes/@statespace/close.m Common: Classes/@statespace/connect.m Common: Classes/@statespace/eig.m Common: Classes/@statespace/get.m Common: Classes/@statespace/getabcd.m Common: Classes/@statespace/getsub.m Common: Classes/@statespace/isempty.m Common: Classes/@statespace/mtimes.m Common: Classes/@statespace/plus.m Common: Classes/@statespace/series.m Common: Classes/@statespace/set.m Common: Classes/@statespace/statespace.m Common: Control/FRespG Common: Graphics/Plot2D
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