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Focuses on study which utilized the structured model reference adaptive control (SMARC) method for the active suppression of limit cycle oscillations for a typical wing section with a structural nonlinearity. Investigation on nonlinear aeroelastic control; Steps in adaptive feedback linearization; Advantages of SMARC over conventional adaptive methods.

Introduces an approach for planning minimum-control optimal trajectories for a two-wheeled mobile robot in the absence of obstacles. Formulation of the trajectory planning in minimum-control, fixed-time and optimal control problems with no terminal cost; Presentation of some of the simulation results of the relaxation method; Solving of the two-point boundary value problem; Discussion of the procedure for constants of motion.