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Further Results on the Input-to-State Stability of a Linear Disturbed System with Control Delay

Mathematics (Basel), 2024-03, Vol.12 (5), p.634

2024

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Active robust control for wing vibrations attenuation

INCAS bulletin, 2022-03, Vol.14 (1), p.209-224

2022

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A Smart Wing Model: From Design to Testing in a Wind Tunnel with a Turbulence Generator

Aerospace, 2024-06, Vol.11 (6), p.493

2024

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Stability for a delayed switched nonlinear system of differential equations in a critical case

International journal of control, 2022-06, Vol.95 (6), p.1543-1550

2022

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Equilibrium stability analysis by numerical simulations for a linear system with time-delayed control

INCAS bulletin, 2019-06, Vol.11 (2), p.179-193

2019

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Advanced Thermal Manikin for Thermal Comfort Assessment in Vehicles and Buildings

Applied sciences, 2022-02, Vol.12 (4), p.1826

2022

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Strain measurements using Fiber Bragg Grating sensors in Structural Health Monitoring

INCAS bulletin, 2017-06, Vol.9 (2), p.77-86

2017

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Flight Envelope Expansion Via Piezoelectric Actuation Receptance Method and Time-delayed Feedback Control

International journal of modeling and optimization, 2019-12, p.317-321

Enciu, Daniela

2019

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New Advances in Space SHM Project

INCAS bulletin, 2015-01, Vol.7 (1), p.65-80

2015

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Lyapunov-Malkin type approach of equilibrium stability in a critical case applied to a switched model of a servomechanism with state delay

International journal of control, 2024-03, Vol.97 (3), p.520-531

2024

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Towards nonconservative conditions for equilibrium stability. Applications to switching systems with control delay

Communications in nonlinear science & numerical simulation, 2023-06, Vol.121, p.107188, Article 107188

2023

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Mathematical modeling of a V-stack piezoelectric aileron actuation

INCAS bulletin, 2016-12, Vol.8 (4), p.141-155

2016

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Equilibrium stability of a nonlinear structural switching system with actuator delay

Journal of the Franklin Institute, 2020-04, Vol.357 (6), p.3680-3701

2020

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Spintronic devices based on graphene nanoribbons with transition metal impurities. Towards space applications

INCAS bulletin, 2014-01, Vol.6 (1), p.45-56

2014

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Magnetic field nanosensor based on Mn impurities

INCAS bulletin, 2014-06, Vol.6 (2), p.51-51

2014

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Damage Identification and Localization in an Aluminium Plate Based on Lamb Waves

International journal of modeling and optimization, 2022-08, p.99-103

2022

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Input‐to‐state stability of a time‐invariant system with control delay and additive disturbances

Proceedings in applied mathematics and mechanics, 2023-12, Vol.23 (4), p.n/a

2023

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New results concerning structural health monitoring technology qualification for transfer to space vehicles

Structural control and health monitoring, 2017-10, Vol.24 (10), p.e1992-n/a

2017

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Numerical and experimental study of circular disc electromechanical impedance spectroscopy signature changes due to structural damage and sensor degradation

Structural health monitoring, 2015-11, Vol.14 (6), p.663-681

2015

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Towards structural health monitoring of space vehicles

Aircraft engineering and aerospace technology, 2017-10, Vol.89 (6), p.920-927

2017

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A problem of stabilization for the mathematical model of electrohydraulic servomechanism with control delay

Journal of the American Romanian Academy of Arts and Sciences, 2019-03, Vol.2 (1)

2019

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Towards Use of Fiber Bragg Grating Sensors for Structural Health Monitoring of (aero)Space Structures

International journal of modeling and optimization, 2018-08, Vol.8 (4), p.246-249

2018

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Flight envelope expansion based on active mitigation of flutter via a V-stack piezoelectric actuator

Journal of physics. Conference series, 2018-10, Vol.1106 (1), p.12033

2018

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THE EVOLVING JURISPRUDENCE OF THE CONSTITUTIONAL COURT REGARDING THE OFFENSE PROVIDED BY THE ARTICLE 6 OF LAW 241/2005

Revista Universul juridic, 2018 (Suplim), p.106-108

Daniela, Enciu

2018

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THE EVOLVING JURISPRUDENCE OF THE CONSTITUTIONAL COURT REGARDING THE OFFENSE PROVIDED BY THE ARTICLE 6 OF LAW 241/2005

Revista Universul juridic, 2016 (Suplim), p.106-108

Daniela, Enciu

2016

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Further Results on the Input-to-State Stability of a Linear Disturbed System with Control Delay

Active robust control for wing vibrations attenuation

A Smart Wing Model: From Design to Testing in a Wind Tunnel with a Turbulence Generator

Stability for a delayed switched nonlinear system of differential equations in a critical case

Equilibrium stability analysis by numerical simulations for a linear system with time-delayed control

Advanced Thermal Manikin for Thermal Comfort Assessment in Vehicles and Buildings

Strain measurements using Fiber Bragg Grating sensors in Structural Health Monitoring

Flight Envelope Expansion Via Piezoelectric Actuation Receptance Method and Time-delayed Feedback Control

New Advances in Space SHM Project

Lyapunov-Malkin type approach of equilibrium stability in a critical case applied to a switched model of a servomechanism with state delay

Towards nonconservative conditions for equilibrium stability. Applications to switching systems with control delay

Mathematical modeling of a V-stack piezoelectric aileron actuation

Equilibrium stability of a nonlinear structural switching system with actuator delay

Spintronic devices based on graphene nanoribbons with transition metal impurities. Towards space applications

Magnetic field nanosensor based on Mn impurities

Damage Identification and Localization in an Aluminium Plate Based on Lamb Waves

Input‐to‐state stability of a time‐invariant system with control delay and additive disturbances

New results concerning structural health monitoring technology qualification for transfer to space vehicles

Numerical and experimental study of circular disc electromechanical impedance spectroscopy signature changes due to structural damage and sensor degradation

Towards structural health monitoring of space vehicles

A problem of stabilization for the mathematical model of electrohydraulic servomechanism with control delay

Towards Use of Fiber Bragg Grating Sensors for Structural Health Monitoring of (aero)Space Structures

Flight envelope expansion based on active mitigation of flutter via a V-stack piezoelectric actuator

THE EVOLVING JURISPRUDENCE OF THE CONSTITUTIONAL COURT REGARDING THE OFFENSE PROVIDED BY THE ARTICLE 6 OF LAW 241/2005

THE EVOLVING JURISPRUDENCE OF THE CONSTITUTIONAL COURT REGARDING THE OFFENSE PROVIDED BY THE ARTICLE 6 OF LAW 241/2005

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