Persona:
Aranda Almansa, Joaquín

Foto de perfil
Dirección de correo electrónico
ORCID
0000-0001-5496-927X
Fecha de nacimiento
Proyectos de investigación
Unidades organizativas
Puesto de trabajo
Apellidos
Aranda Almansa
Nombre de pila
Joaquín
Nombre

Filtros

2003 - 20077
Restablecer filtros

Ajustes

Fecha de inicio: 2000 × Tipo: book part ×

Resultados de la búsqueda

Mostrando 1 - 7 de 7
  • Miniatura
    Publicación
    Interactive software tools for robust control: application to marine systems
    (Robotics and Automation in the Maritime Industries, 2006-01-01) Dormido Bencomo, Sebastián; Díaz Martínez, José Manuel; Aranda Almansa, Joaquín; Dormido Canto, Sebastián; Muñoz Mansilla, María del Rocío; Chaos García, Dictino
  • Miniatura
    Publicación
    An Overview about Dynamic Positioning of Ships
    (Automation for the Maritime Industries, 2004-01-01) Hernández Cuesta, Carlos; Aranda Almansa, Joaquín; Díaz Martínez, José Manuel; Dormido Canto, Sebastián; Muñoz Mansilla, María del Rocío
  • Miniatura
    Publicación
    Automation for the Maritime Industries
    (2007-11-12) Armada, Manuel A.; Cruz García, Jesús Manuel de la; Aranda Almansa, Joaquín
  • Miniatura
    Publicación
    ROLL MODEL FOR CONTROL OF A FAST FERRY
    (Olivella Puig J.; García Carcellé V.; García Domingo E., 2003-01-01) Aranda Almansa, Joaquín; Díaz Martínez, José Manuel; Muñoz Mansilla, María del Rocío
  • Miniatura
    Publicación
    Non Linear Dynamic Inversion Technique
    (GROUP FOR AERONAUTICAL RESEARCH AND TECHNOLOGY IN EUROPE, 2007-11-12) Aranda Almansa, Joaquín
    Over the last two decades or so, control researchers have begun to apply alternative methodologies to flight control design. One alternative is variously called non-linear dynamic inversion or feedback linearization. The purpose of dynamic inversion is to develop a feedback control law that linearizes the plant response to commands. Simple controllers can then be designed. With dynamic inversion, a non-linear control law is designed which globally reduces the dynamics of selected controlled variables to integrators. A closed loop system is then designed to make the controlled variables exhibit specified command responses while satisfying the usual disturbances response and robustness requirements for the overall system and the various physical limitations of the aircraft’s control effectors.
  • Miniatura
    Publicación
    About Identification of Mathematical Models for High Speed Crafts
    (Automation for the Maritime Industries, 2004-01-01) Dormido Bencomo, Sebastián; Muñoz Mansilla, María del Rocío; Aranda Almansa, Joaquín; Díaz Martínez, José Manuel; Dormido Canto, Sebastián
  • Miniatura
    Publicación
    Control problems in marine vehicles: Some experiences in stabilization and tracking control
    (2006-01-01) Cruz García, Jesús Manuel de la; Riola Rodríguez, José María; Aranda Almansa, Joaquín; Muñoz Mansilla, María del Rocío; Chaos García, Dictino; Díaz Martínez, José Manuel; Dormido Canto, Sebastián