The optimal control and stabilization of nonlinear systems of the form x˙ = A(x)x + B(x)u is considered and explicit expressions for the control are developed. Excellent results have been obtained when we apply the technique presented here to an anaytical nonlinear model of the F-8 fighter aircraft.
No takes yet. Share an insight, caveat, or question.
Banks et al. (1992) studied this question.
Synapse has enriched 5 related papers. Consider them for comparative context: