Path: AC/Aircraft
% Find the equilibrium state of the engine. -------------------------------------------------------------------------- Form: x = ACEngEq( d, v, r ) -------------------------------------------------------------------------- ------ Inputs ------ d Aircraft data v (3,1) Velocity r (3,1) Position ------- Outputs ------- x Equilibrium engine state -------------------------------------------------------------------------- See also Altitude, AirData, ACEngine --------------------------------------------------------------------------
AC: ACActuator/ACThrust AC: Aircraft/ACEngine AerospaceUtils: AeroData/AtmData AerospaceUtils: AtmosphericCalculations/AirData Common: Atmosphere/StdAtm 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/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS Common: Transform/Altitude Math: Analysis/IntExt Math: Linear/Mag
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