Path: ACPro/Trajectory
% EquilibriumControls finds controls to maintain equilibrium. For a point mass aircraft. Calls RHSPointMassAircraft via fminsearch. Type EquilibriumControls for a demo. -------------------------------------------------------------------------- Form d = EquilibriumControls( x, d ) -------------------------------------------------------------------------- ------ Inputs ------ x (6,1) State [v;gamma;psi;xE;yN;h] d (.) Data structure see RHSPointMassAircraft ------- Outputs ------- d (.) Data structure see RHSPointMassAircraft --------------------------------------------------------------------------
ACPro: Trajectory/RHSPointMassAircraft
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