Some directs numerical methods for solving the nonlinear optimal control problem practical in aeronautic

  • Aliane Mohamed University Amar Telidji of Laghouat, Algeria
  • Nacima Moussouni
Keywords: Optimal Control, Euler discretization, Rung kutta method, active-set method, aerodynamic

Abstract

In this study, we have implemented direct numerical methods to convert the continuous optimal control problem into a nonlinear optimization problem. We used three discretization techniques: the Euler method, the second-order Runge-Kutta method, and the fourth-order Runge-Kutta method. Subsequently, the resulting non-linear optimization problem was solved using MATLAB's fmincon function. To evaluate the efficiency and accuracy of the proposed approach, we modeled a nonlinear optimal control problem relevant to aeronautics. Our objective was to minimize the travel time of a rocket from an initial point to a final point at a specified altitude, considering aerodynamic forces and gravity, with the control variable being the rocket's heel angle. To compare the different methods, we developed a MATLAB implementation and showcased various simulation results.
Published
2024-09-07
How to Cite
Mohamed, A., & Moussouni, N. (2024). Some directs numerical methods for solving the nonlinear optimal control problem practical in aeronautic. Statistics, Optimization & Information Computing. https://doi.org/10.19139/soic-2310-5070-1440
Section
Research Articles

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