| Titre : | Applied min-max approach to missile guidance and control |
| Auteurs : | Shaul Gutman |
| Type de document : | Books |
| Editeur : | Reston : The American Institute of Aeronautics and Astronautics, 2005 |
| Article en page(s) : | XVII, 98 p. |
| Collection : | Progress in astronautics and aeronautics, ISSN 0079-6050, num. 209 |
| ISBN/ISSN/EAN : | 978-1-56347-695-2 |
| Langues: | Anglais |
| Index. décimale : | 629.8312 |
| Tags : | Guided missiles--Guidance systems ; Control theory ; Guided missiles--Control systems |
| Résumé : |
This book is concerned with dynamical systems under a large uncertainty, and uses a min-max approach to achieve worst-case design.The book consits of two parts .The first part deals with robust control. It begins by developing linear controls to achieve relative stability (pole clustering) under parameter space is sometimes discontinuous (fragile) with respect to the control parameters.Then, the book discusses the control of nonlinear uncertain systems under maching conditions.The second part uses differntial games to develop optimal guidance for homing missiles against maneuvering targets.The target maneuver is bounded, but otherwise arbitrary.Using miss distance as the cost, the book develops closed form guidance laws, as well as miss distance formulae.In this way,the control loop (autopilot) and the guidance loop are coupled.A parameter study reveals the basic difference between minimum phase (canards) and non-minimum phase. |
Exemplaires (1)
| Code-barres | Cote | Support | Localisation | Section | Disponibilité |
|---|---|---|---|---|---|
| 100960R | ABAL 623.463 | Book | Royal Military Academy | Systèmes d’Armes et Balistique | Disponible |
