Path: Airships/Analysis
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Obtain the linear model of an airship at a particular flight condition.
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Form:
[g,gLat,gLon] = GetAirshipLinMod( name, h, V, theta )
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Inputs
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name (:) Name of linear model mat-file.
(see "GenerateAirshipLinMods.m")
h (1) Altitude [m]
V (1) Total velocity [m/s]
theta (1) Pitch [rad]
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Outputs
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g (.) Full state linear model, statespace class
Additional outputs optional: (see "AirshipStatespace.m")
gLat (.) Lateral-Directional linear model
gLon (.) Longitudinal linear model
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Airships: Control/AirshipStatespace 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/Append Common: Control/Parallel Common: Control/Series Common: Control/SizeABCD Common: General/CellToMat
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