Compuation of Real-Time-Control in Aerospace Applications by Multiple Shooting Procedures

Extended Abstract

Let the problem of optimal control be defined as

$$ {\rm{\dot \eta = \Phi }}\left( {{\rm{t,\eta ,u}}} \right){\rm{ , }}{{\rm{t}}_{\rm{o}}} \le {\rm{t}} \le {{\rm{t}}_{\rm{e}}} $$

((1))

with boundary conditions for the state variable η(t) at t = t_o and t = t_e, t_e fixed or free, u(t) is the control; the quantity to be optimized is denoted by Ф(t_e, η(t_e)).

Full manuscript to be published later in a periodical.