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control of the longitudinal dynamics of the F16 aeroplane
Longitudinal instrument landing system design using both Eigenstructure
Associative memories as learning basis applied to the roll control
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achieved actuator analysis applied approach batch behaviour bottle cascade chemotaxis closed-loop system coefficient control algorithm control design control loops control strategy controlled variables decoupling developed diagonal eigenvalues elements Engineering equation error estimation feedback Figure flow rate frequency fuzzy controller gain heat Hough transform implemented initial injection moulding input integral interaction linear MATLAB maximum measurement method milk model predictive control model-following monomer monomer conversion moulding process multivariable control nonlinear control nonlinear systems obtained on-line open loop operating optimal control optimal temperature paper parameter performance perturbed phugoid PI controllers plant polymer polymerisation predictive control pressure procedure process control reactor reduced relative humidity robust control robust stability roll sampling setpoint shown in Fig simulation SIMULINK speed step response structure tank techniques tracking transfer function matrix transputer tuning ultrasound uncertainty University of Bradford values variation velocity