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Path: AC/Aero
% Implements the "Air Data Computer" model. -------------------------------------------------------------------------- Form: [aMach, qBar] = ADC( vT, alt ) -------------------------------------------------------------------------- ------ Inputs ------ vT (1,1) Velocity (ft/sec) alt (1,1) Altitude (ft) ------- Outputs ------- aMach (1,1) Mach Number qBar (1,1) Dynamic pressure --------------------------------------------------------------------------
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