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Path: AC/Aircraft
% Find the equilibrium state of the engine. Since version 2 (ACT) -------------------------------------------------------------------------- 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: Aircraft/ACEngine AerospaceUtils: AtmosphericCalculations/AirData Common: Transform/Altitude Math: Linear/Mag
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