Path: AC/ACDynamics
% Plots the aircraft data. opt is 'info', 'init', 'store', 'plot'
If opt is 'info' d is a list of plots. Otherwise it is
the d returned from ACPlot. The calls are
d = ACPlot( x, 'init', plots, g, nPts, dT, nSim )
do k = 1:nSim
d = ACPlot( x, 'store', d, control )
end
ACPlot( x, 'plot', d )
Possible plots are:
Altitude
Euler angles
Quaternion
Angular rate
Position ECI
Velocity
Alpha (also get beta and total velocity)
Mass
Inertia
CG
Engine states
Actuator states
Sensor states
Flex model states
Disturbance model states
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Form:
d = ACPlot( x, opt, d, g, nPts, dT, nSim )
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------
Inputs
------
x (:) Aircraft state vector or 'plot' if opt is 'store'
opt (n,:) Options 'info'
'init'
'store'
'plot'
d (:) Internal data structure or list of plots
g (:) Aircraft data structure or d.control when opt = 'store'
nPts (1,1) Number of plot steps
dT (1,1) Sim time step
nSim (1,1) Number of sim steps
units (1,:) Units
-------
Outputs
-------
d (:) Internal data structure or list of plots
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AC: ACCoord/AlphBeta AC: ACCoord/ECIToNED AC: ACCoord/EulNED Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/DeBlankLT Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Graphics/TimeLabl Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS Common: Quaternion/Mat2Q Common: Quaternion/Q2Eul Common: Quaternion/Q2Mat Common: Quaternion/QMult Common: Quaternion/QPose Common: Transform/Altitude Common: Transform/Mat2Eul Math: Linear/Mag
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