Optimal Control of Aerospace Systems with Control-State Constraints and Delays

Optimal control, parabolic equations, box constraints for the control, finitely many con- straints for the state, Robinson constraint qualification, second order optimality

Abstract: This paper provides an analysis of Pontryagine mimina satisfying a quadratic growth condition, for optimal control problems of ordinary differential equations with

Energy-optimal drive control under several scenarios (acceleration, decelera- tion, driving between stops, approaching traffic lights, cruise within a speed band) [3] can be treated

Bergounioux, Optimal control of abstract elliptic variational inequalities with state constraints,, to appear, SIAM Journal on Control and Optimization, Vol. Tiba, General

The idea proposed in this paper consists in introducing a general method that allows to solve successfully (OCP) τ using indirect methods combined with homotopy procedures, with τ

We first penalize the state equation and we obtain an optimization problem with non convex constraints, that we are going to study with mathematical programming methods once again

Earth-Moon transfer, low thrust, circular restricted three-body problem, optimal control, minimum time or fuel consumption trajectories, shoot- ing, discrete and

However, one should not switch to a lower drift regime unless it lowers the firm’s bankruptcy risk. It may happen, when the value firm dangerously approaches bankruptcy threshold,