Michael I. Friswell
Swansea University
762 Papers
4.5K Citations
Michael I. Friswell is an academic researcher from Swansea University. The author has contributed to research in topics: Finite element method & Morphing. The author has an hindex of 73, co-authored 724 publications. Previous affiliations of Michael I. Friswell include Imperial College London & College of Engineering, Trivandrum.
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Papers
Optimization of anisotropic composite panels with T-shaped stiffeners including transverse shear effects and out-of-plane loading
TL;DR: In this article, a two-step method to optimize anisotropic composite panels with T-shaped stiffeners, including a new formulation of the transverse shear properties and an approximation of the ply contiguity (blocking) constraints as functions of the lamination parameters is provided.
Distributed Modal Sensors for Rectangular Plate Structures
Kailin Jian,Michael I. Friswell +1 more
TL;DR: In this article, the authors considered the design of distributed modal sensors for plate structures, where sensors are assumed to be of constant thickness and the modes of the plate are known functions.
The use of model updating for reliable finite element modelling and fault diagnosis of structural components used in nuclear plants
TL;DR: In this article, the authors present an overview of model updating and its use in fault diagnosis, using typical examples, focusing on the usefulness of the updating method, rather than describing the different updating methods in detail.
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Finite element model updating using Hamiltonian Monte Carlo techniques
TL;DR: The shadow HMC technique (SHMC), which is a modified version of the HMC method, was developed to improve sampling for large system sizes by drawing from a modified shadow Hamiltonian function, but the SHMC algorithm performance is limited by the use of a non-separable modified Hamiltonianfunction.
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Robust Fault Tolerant Control for Spacecraft Attitude Stabilization Under Actuator Faults and Bounded Disturbance
TL;DR: In this article, the authors investigated the design of spacecraft attitude stabilization controllers that are robust against actuator faults and external disturbances and showed that the attitude orientation and angular velocity of the closed-loop system asymptotically converge to zero when the actuators are fault-free.
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