| Titre : | Partial stabilization approach to 3-dimensional guidance law design (2012) |
| Auteurs : | T. Binazadeh, Auteur ; Yazdanpanah, M. J., Auteur |
| Type de document : | Article : texte imprimé |
| Dans : | Transactions of the ASME . Journal of dynamic systems, measurement, and control (Vol. 133 N° 6, Novembre 2011) |
| Article en page(s) : | 04 p. |
| Note générale : | Dynamic systems |
| Langues : | Anglais |
| Index. décimale : | 553 (Géologie économique. Minérographie. Minéraux. Formation et gisements de minerais) |
| Tags : | Missile guidance Robust control Variable structure systems Vehicle dynamics |
| Résumé : | In this paper, a new approach to design the 3-dimensional missile guidance law, based on partial stabilization, is presented. The approach is based on the classification of the state variables within the guidance system dynamics with respect to their required stabilization properties. The resulting guidance law enables the missile to intercept highly maneuvering targets within a finite interception time. Effectiveness of the proposed guidance law is demonstrated through analysis and simulations. |
| DEWEY : | 553 |
| ISSN : | 0022-0434 |
| En ligne : | http://www.asmedl.org/getabs/servlet/GetabsServlet?prog=normal&id=JDSMAA000133000006064504000001&idtype=cvips&gifs=Yes&ref=no |
