Flight control algorithm design with multiobjective parameter synthesis

This paper addresses the problem of finding optimum parameters for a given controller with the given conflicting goals, including the nonlinear agility criterion for the first time in the literature, and proposes compromise decision support problem (cDSP) method for the first time in order to optimize the multi objective controller synthesis problem. Here the conflicting goals are combined together for the optimization problem. In the last section of the paper, the benefits of the using multi objective optimization will be shown on controlling an aircraft in longitudinal axis.