Iterative Learning Control for homing guidance design of missiles
This paper presents an Iterative Learning Control design applied to homing guidance of missiles against maneuvering targets. According to numerical experiments, although an increase of the control energies is appreciated with respect to a previous published base controller for comparison, this strat...
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| Tipo de recurso: | artículo |
| Fecha de publicación: | 2017 |
| País: | España |
| Institución: | Universitat Politècnica de Catalunya (UPC) |
| Repositorio: | UPCommons. Portal del coneixement obert de la UPC |
| Idioma: | inglés |
| OAI Identifier: | oai:upcommons.upc.edu:2117/109686 |
| Acceso en línea: | https://hdl.handle.net/2117/109686 https://dx.doi.org/10.1016/j.dt.2017.01.002 |
| Access Level: | acceso abierto |
| Palabra clave: | Control theory Iterative methods (Mathematics) Terminal guidance law Missiles Iterative learning control Control automàtic Àrees temàtiques de la UPC::Matemàtiques i estadística |
| Sumario: | This paper presents an Iterative Learning Control design applied to homing guidance of missiles against maneuvering targets. According to numerical experiments, although an increase of the control energies is appreciated with respect to a previous published base controller for comparison, this strategy, which is simple to realize, is able to reduce the time to reach the head-on condition to target destruction. This fact is important to minimize the missile lateral force-level to fulfill engaging in hypersonic target persecutions. |
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