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Designing a Biomimetic Ornithopter Capable of Sustained and Controlled Flight

Journal of bionics engineering, 2008-03, Vol.5 (1), p.39-47

2008

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Bird-mimetic Wing System of Flapping-wing Micro Air Vehicle with Autonomous Flight Control Capability

Journal of bionics engineering, 2016-07, Vol.13 (3), p.458-467

2016

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Lookup table control method for vibration suppression of a flexible manipulator with optimization of the minimum settling time and energy consumption

Asian journal of control, 2012-05, Vol.14 (3), p.693-706

2012

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Aerodynamic forces and flow structures of the leading edge vortex on a flapping wing considering ground effect

Bioinspiration & biomimetics, 2013-09, Vol.8 (3), p.036007-036007

2013

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Flow structures around a flapping wing considering ground effect

Experiments in fluids, 2013-07, Vol.54 (7), p.1-19, Article 1575

2013

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Piezo-composite actuated control surface system for flying vehicle

Aircraft Engineering and Aerospace Technology, 2010-10, Vol.82 (6), p.372-375

2010

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Non-Jumping Take off Performance in Beetle Flight (Rhinoceros Beetle Trypoxylus dichotomus)

Journal of bionics engineering, 2014-01, Vol.11 (1), p.61-71

2014

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Design and Development of a Class of Rotorcraft-Based UAV

International journal of advanced robotic systems, 2013-02, Vol.10 (2)

2013

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The durability of a conducting shape memory polyurethane actuator

Smart materials and structures, 2007-08, Vol.16 (4), p.N23-N26

2007

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Two- and Three-Dimensional Simulations of Beetle Hind Wing Flapping during Free Forward Flight

Journal of bionics engineering, 2013-07, Vol.10 (3), p.316-328

2013

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압축 응력 변화에 대한 압전 단결정의 물성 변화를 고려한 압전 복합재료 작동기의 작동 변위 예측

Composites Research, 2017, 30(1), , pp.15-20

2017

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Analytical model and optimal design of a d33-mode active layer for the lightweight unimorph piezo-composite actuator

Journal of electroceramics, 2011-06, Vol.26 (1-4), p.175-184

2011

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Improvement of the Parameterized Identification Model Using Quasi-Steady and Nonuniform Inflow Aerodynamic Model

Journal of aerospace engineering, 2011-07, Vol.24 (3), p.378-388

2011

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Design and demonstration of a biomimetic wing section using a lightweight piezo-composite actuator (LIPCA)

Smart materials and structures, 2005-08, Vol.14 (4), p.496-503

2005

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Three-dimensional cure simulation of composite structures by the finite element method

Composite structures, 2003-10, Vol.62 (1), p.51-57

2003

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Mimicking a Superhydrophobic Insect Wing by Argon and Oxygen Ion Beam Treatment on Polytetrafluoroethylene Film

Journal of bionics engineering, 2009-12, Vol.6 (4), p.365-370

2009

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Actuation characterization of the lightweight unimorph piezo-composite actuator for different loading cases

Advanced composite materials, 2013-06, Vol.22 (3), p.203-212

2013

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소형 무인 비행체 조종면 작동용 압전 복합재료 작동기 연구

Composites Research, 2014, 27(2), , pp.47-51

2014

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Control system design and testing for a small-scale autonomous helicopter

Aircraft Engineering and Aerospace Technology, 2010-10, Vol.82 (6), p.353-359

2010

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Instrumented flight test of flapping micro air vehicle

Aircraft Engineering, 2013-01, Vol.85 (4), p.326-339

2013

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Design Analysis of a 3-3 Mode Piezocomposite Actuator

Advanced composite materials, 2011-01, Vol.20 (4), p.301-317

2011

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FATIGUE BEHAVIOR DEGRADATION DUE TO THE INTERLAMINAR CONDITIONS IN LIGHTWEIGHT PIEZOELECTRIC COMPOSITE ACTUATOR (LIPCA)

International journal of modern physics. B, Condensed matter physics, statistical physics, applied physics, 2006-10, Vol.20 (25n27), p.4365-4370

2006

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A nine-node assumed strain shell element for analysis of a coupled electro-mechanical system

Smart materials and structures, 2003-06, Vol.12 (3), p.355-362

2003

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A Study on the Actuating Performance of Unimorph Piezoelectric Actuators with a Center Load

Key engineering materials, 2006-12, Vol.326-328, p.1411-1414

2006

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The effect of electro-mechanical coupling stiffness on the through-the-thickness electric potential distribution of piezoelectric actuators

Smart materials and structures, 2005-08, Vol.14 (4), p.754-758

2005

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Designing a Biomimetic Ornithopter Capable of Sustained and Controlled Flight

Bird-mimetic Wing System of Flapping-wing Micro Air Vehicle with Autonomous Flight Control Capability

Lookup table control method for vibration suppression of a flexible manipulator with optimization of the minimum settling time and energy consumption

Aerodynamic forces and flow structures of the leading edge vortex on a flapping wing considering ground effect

Flow structures around a flapping wing considering ground effect

Piezo-composite actuated control surface system for flying vehicle

Non-Jumping Take off Performance in Beetle Flight (Rhinoceros Beetle Trypoxylus dichotomus)

Design and Development of a Class of Rotorcraft-Based UAV

The durability of a conducting shape memory polyurethane actuator

Two- and Three-Dimensional Simulations of Beetle Hind Wing Flapping during Free Forward Flight

압축 응력 변화에 대한 압전 단결정의 물성 변화를 고려한 압전 복합재료 작동기의 작동 변위 예측

Analytical model and optimal design of a d33-mode active layer for the lightweight unimorph piezo-composite actuator

Improvement of the Parameterized Identification Model Using Quasi-Steady and Nonuniform Inflow Aerodynamic Model

Design and demonstration of a biomimetic wing section using a lightweight piezo-composite actuator (LIPCA)

Three-dimensional cure simulation of composite structures by the finite element method

Mimicking a Superhydrophobic Insect Wing by Argon and Oxygen Ion Beam Treatment on Polytetrafluoroethylene Film

Actuation characterization of the lightweight unimorph piezo-composite actuator for different loading cases

소형 무인 비행체 조종면 작동용 압전 복합재료 작동기 연구

Control system design and testing for a small-scale autonomous helicopter

Instrumented flight test of flapping micro air vehicle

Design Analysis of a 3-3 Mode Piezocomposite Actuator

FATIGUE BEHAVIOR DEGRADATION DUE TO THE INTERLAMINAR CONDITIONS IN LIGHTWEIGHT PIEZOELECTRIC COMPOSITE ACTUATOR (LIPCA)

A nine-node assumed strain shell element for analysis of a coupled electro-mechanical system

A Study on the Actuating Performance of Unimorph Piezoelectric Actuators with a Center Load

The effect of electro-mechanical coupling stiffness on the through-the-thickness electric potential distribution of piezoelectric actuators

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