1. An Indirect Method for Optimal Guidance of a Glider
- Author
-
R. Pepy, Bruno Hérissé, ONERA - The French Aerospace Lab [Palaiseau], ONERA-Université Paris Saclay (COmUE), and Hérissé, Bruno
- Subjects
020301 aerospace & aeronautics ,0209 industrial biotechnology ,Engineering ,Missile guidance ,business.industry ,Differential equation ,Optimal path ,Glider ,02 engineering and technology ,Optimal control ,System of linear equations ,[SPI.AUTO]Engineering Sciences [physics]/Automatic ,Set (abstract data type) ,[SPI.AUTO] Engineering Sciences [physics]/Automatic ,020901 industrial engineering & automation ,Shooting method ,0203 mechanical engineering ,Terminal (electronics) ,Control theory ,Trajectory ,business - Abstract
International audience; This paper addresses the problem of finding the trajectory, for a glider, that maximizes the final velocity and respect both initial and terminal conditions on the state. A new set of differential equations governing the system, deduced using optimal control theory, is proposed. To solve this system of equations, an algorithm based on an indirect shooting method is described. It provides paths for which the final speed is higher than the one obtained by a current common closed-loop method.
- Published
- 2014