Model Development and Optimization for Space Engineering: Concepts, Tools, Applications, and Perspectives

Model predictive control for reusable space launcher guidance improvement

“…2 with xk i-1 , uk i-1 and the matrices; 2. Store the new solution xk i , uk i , Δ i , νk i ; The algorithm has been validated by applying the method to a nonlinear optimal control problem of which it is known the analytical solution [9], [11], [12].…”

“…The rotational motion is governed by Euler rigidbody attitude dynamics: (11) Ω(.) is the skew-symmetric matrix of the angular velocities, while J is the inertia matrix.…”