Multi-objective controller design via optimal interpolation with anaircraft control application

摘要

In this paper, a controller design methodology is proposed tosatisfy a set of closed-loop objectives simultaneously. The set ofobjectives consists of: 1) pole placement, 2) decoupled command trackingof step inputs at steady-state, and 3) minimization of step responsetransients with respect to envelope specifications. The proposedmulti-objective control is applied to a simplified lateral/directionaldynamics of an L-1011 aircraft at cruise flight conditions