Path: AC/Aircraft
% Aircraft engine model.
Uses a piecewise linear model to map throttle to commanded power and a
lag to model the response of the throttle to the input command.
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Form:
g = ACEngine( x, d, control, altitude, machNo )
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Inputs
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x State
d Engine data
control Controls
machNo (1,1) Mach number
altitude (1,1) Altitude
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Outputs
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g Output data structure
.torque (3,1) Core torques
.force (3,1) Core forces
.xDot (:,1) Engine state derivatives
.mDot (1,1) Fuel consumption
.inertiaDot (3,3) Inertia derivative due to fuel consumption
.cGDot (3,1) CG derivative due to fuel consumption
.torqueRotor (:,1) Torques on rotors
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See also ACThrust
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AC: ACActuator/ACThrust Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Math: Analysis/IntExt
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