This article presents and validates a general framework to build a linear dynamic Finite Element-based model of large exible structures for integrated Control/Structure design. An extension of the Two-Input Two-Output Port (TITOP) approach is here developed. The authors had already proposed such framework for simple beam-like structures: each beam was considered as a TITOP sub-system that could be interconnected to another beam thanks to the ports. The present work studies bodies with multiple attaching points by allowing complex interconnections among several sub-structures in tree-like assembly. The TITOP approach is extended to generate NINOP (N-Input N-Output Port) models. A Matlab toolbox is developed integrating beam and bending plate...
Viscoelastic materials are often characterized by a completely monotone kernel : this gives rise to ...
Multi-core, and Time and Space Partitionnong sys- tems are two emerging paradigms for architecting a...
One of the important issues in the certification of composite aeronautical structures is large notch...
International audienceThe port-Hamiltonian formulation is a powerful method for modeling and interco...
Methods for discretizing port-Hamiltonian systems are of interest both for simulation and control pu...
This paper proposes a novel dynamic model of a Reaction Wheel Assembly (RWA) based on the Two-Input ...
The Kirchhoff plate model is detailed by using a tensorial port-Hamiltonian (pH) formulation. A stru...
A port-Hamiltonian formulation for general linear coupled thermoelasticity and for the thermoelastic...
Many applications in structural mechanics require the numerical solution of sequences of linear syst...
In this brief, we develop a mathematical model of a flexible spacecraft system composed of a hub and...
The mechanical model of a thin plate with boundary control and observation is presented as a port-Ha...
International audienceThe cohesive zone modelling (CZM) is extensively used for the simulation of de...
We consider the design of structure-preserving discretization methods for the solution of systems of...
Adhesively bonded joints are often addressed through Finite Element (FE). However, analyses based on...
A new formulation for the modular construction of flexible multibody systems is presented. By rearra...
Viscoelastic materials are often characterized by a completely monotone kernel : this gives rise to ...
Multi-core, and Time and Space Partitionnong sys- tems are two emerging paradigms for architecting a...
One of the important issues in the certification of composite aeronautical structures is large notch...
International audienceThe port-Hamiltonian formulation is a powerful method for modeling and interco...
Methods for discretizing port-Hamiltonian systems are of interest both for simulation and control pu...
This paper proposes a novel dynamic model of a Reaction Wheel Assembly (RWA) based on the Two-Input ...
The Kirchhoff plate model is detailed by using a tensorial port-Hamiltonian (pH) formulation. A stru...
A port-Hamiltonian formulation for general linear coupled thermoelasticity and for the thermoelastic...
Many applications in structural mechanics require the numerical solution of sequences of linear syst...
In this brief, we develop a mathematical model of a flexible spacecraft system composed of a hub and...
The mechanical model of a thin plate with boundary control and observation is presented as a port-Ha...
International audienceThe cohesive zone modelling (CZM) is extensively used for the simulation of de...
We consider the design of structure-preserving discretization methods for the solution of systems of...
Adhesively bonded joints are often addressed through Finite Element (FE). However, analyses based on...
A new formulation for the modular construction of flexible multibody systems is presented. By rearra...
Viscoelastic materials are often characterized by a completely monotone kernel : this gives rise to ...
Multi-core, and Time and Space Partitionnong sys- tems are two emerging paradigms for architecting a...
One of the important issues in the certification of composite aeronautical structures is large notch...