Distributed Attitude Consensus of Multiple Flexible Spacecraft [electronic resource] / by Ti Chen, Jinjun Shan, Hao Wen.

Por: Chen, Ti [author.]Colaborador(es): Shan, Jinjun [author.] | Wen, Hao [author.] | SpringerLink (Online service)Tipo de material: TextoTextoEditor: Singapore : Springer Nature Singapore : Imprint: Springer, 2023Edición: 1st ed. 2023Descripción: XV, 210 p. 101 illus., 100 illus. in color. online resourceTipo de contenido: text Tipo de medio: computer Tipo de portador: online resourceISBN: 9789811942587Tema(s): Aerospace engineering | Astronautics | Control engineering | Robotics | Automation | Aerospace Technology and Astronautics | Control, Robotics, AutomationFormatos físicos adicionales: Printed edition:: Sin título; Printed edition:: Sin título; Printed edition:: Sin títuloClasificación CDD: 629.1 Clasificación LoC:TL1-4050Recursos en línea: Libro electrónicoTexto
Contenidos:
Introduction -- Attitude Dynamics -- Distributed Attitude Tracking Based on 3-Dimensional Attitude Representations -- Distributed Attitude Tracking on SO(3) Under Undirected Graphs -- Distributed Attitude Tracking on SO(3) Under Directed Graphs -- Leaderless Attitude Consensus on SO(3).
En: Springer Nature eBookResumen: This book mainly presents the authors' recent studies on the distributed attitude consensus of multiple flexible spacecraft. Modified Rodrigues parameters and rotation matrix are used to represent spacecraft attitude. Several distributed adaptive controllers are presented with theoretical analyses, numerical simulations and experimental verifications. The authors intend to provide a manual that allows researchers, engineers and students in the field of aerospace engineering and mechanics to learn a theoretical and practical approach to the design of attitude consensus algorithms.
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Acceso multiusuario

Introduction -- Attitude Dynamics -- Distributed Attitude Tracking Based on 3-Dimensional Attitude Representations -- Distributed Attitude Tracking on SO(3) Under Undirected Graphs -- Distributed Attitude Tracking on SO(3) Under Directed Graphs -- Leaderless Attitude Consensus on SO(3).

This book mainly presents the authors' recent studies on the distributed attitude consensus of multiple flexible spacecraft. Modified Rodrigues parameters and rotation matrix are used to represent spacecraft attitude. Several distributed adaptive controllers are presented with theoretical analyses, numerical simulations and experimental verifications. The authors intend to provide a manual that allows researchers, engineers and students in the field of aerospace engineering and mechanics to learn a theoretical and practical approach to the design of attitude consensus algorithms.

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