test 관리자 test

Welcome to "Space Structures and H/W Systems Laboratory". 우주시스템 분야에서는 우주발사체, 위성 개발 및 활용, 우주 과학 및 탐사와 관련된 연구들을 수행해 오고 있다. 이 분야의 대표적인 연구 주제로 다음과 같은 것들이 있다.
과학로켓개발
큐브위성 시스템 개발 (2017년 국내 최초로 교신 성공): Little Intelligent Nanosatellite of KAIST (LINK)
위성항법시스템 (Global Navigation Satellite System, GNSS) 관련 연구, 이를 활용한 각종 우주 과학 연구
달 탐사를 위한 위험 감지 및 회피 기술 적용 착륙 연구 (Autonomous Landing and Hazard Avoidance Technology, ALHAT)
우주 발사체 개념 설계를 위한 범용 비행 분석 프로그램 개발 연구

우주시스템 분야에서는 우주발사체, 위성 개발 및 활용, 우주 과학 및 탐사와 관련된 연구들을 수행해 오고 있다. 이 분야의 대표적인 연구 주제로 다음과 같은 것들이 있다.
과학로켓개발
큐브위성 시스템 개발 (2017년 국내 최초로 교신 성공): Little Intelligent Nanosatellite of KAIST (LINK)
위성항법시스템 (Global Navigation Satellite System, GNSS) 관련 연구, 이를 활용한 각종 우주 과학 연구
달 탐사를 위한 위험 감지 및 회피 기술 적용 착륙 연구 (Autonomous Landing and Hazard Avoidance Technology, ALHAT)
우주 발사체 개념 설계를 위한 범용 비행 분석 프로그램 개발 연구

New Folding Concept on the Cylindrical Structure with Yoshimura Pattern: Folding pattern analysis

Improved aerodynamic model for efficient analysis of flapping-wing flight

Thermal post-buckling analysis of shape memory alloy hybrid composite shellpanels

Establishment of gun blast wave model and structural analysis for blast load

Wing-Wake Interaction of Insect-Like Flapping Wing in Hover: Effect of Aspect Ratio and Kinematics at Re~104

WING-WAKE INTERACTION OF INSECT-LIKE FLAPPING WING IN HOVER: EFFECT OF ASPECT RATIO AND KINEMATICS AT RE~ 𝟏𝟎𝟒

외부장착물이 있는 항공기 날개의 플러터 특성 및 능동 진동 제어

Torsion-Induced Compliant Joints and its Application to Flat-Foldable and Self-Assembling Robotic Arm

Flutter Characteristics and Active Vibration Control of Aircraft Wing with External Store

A Sizing Method for Solar Power Long Endurance UAVs

Design of High-precision CTE measurement System for the Structural Materials in Space Applications

Mathematical separation behavior modeling for the split-type separation device

Vibration Control of the Composite Wing Model Using Piezoelectric Actuators

A multibody approach for 6-DOF flight dynamics and stability analysis of the hawkmoth Manduca sexta

탄소나노섬유와 NiFe 분말을 함유한 전자기파 흡수재료

볼타입 분리볼트 분리 메커니즘의 수치해석 및 간략화 모델링

스플릿 타입 분리장치의 수학적 동적 분리 거동 모델링

The Trim Condition of a Hovering Insect-like Flapping-wing Micro Air Vehicle in Asymmetric Condition

스핀테이블을 이용한 스핀안정화 기법 연구

Aeroelastic analysis of a wing with freeplay in the subsonic/transonic regions

Numerical investigation on the aeroelastic instability of a complete aircraft model

우주용 구조 재료의 초정밀 열팽창계수 측정시스템 설계

Dynamic model establishment of a deployable missile control fin with nonlinear hinge

Measurement of rotor blade deformation and motions using stereo pattern recognition method

Large deformation analysis of inflated membrane boom structures with various slenderness ratios

Finite element analysis of adaptive inflatable structures with SMA strip actuator

A thickness-accommodating method for void-free design in uniformly thick origami

Experimental evaluation of spacecraft RWA disturbance with flexible structural effects

Wrinkling control of inflatable booms using smart material patch

Smart flapping wing using macrofiber composite actuators

Interactions of the wakes of two flapping wings in hover

Control of wing stroke plane angle for stabilizing of a hovering flapping-wing air vehicle

Aeroelastic Analysis of Two-Dimensional Tandem Wing using Vortex Lattice Method

Notch filter 제어기법을 이용한 반작용 휠 미소진동 절연장치의 절연성능 평가

Multidisciplinary design optimization of the flapping-wing air vehicle using artificial neural network surrogate model

다양한 날개/외부 장착물 조합에 따른 플러터 특성평가

An investigation of 6-DOF insect flight dynamics with a flexible multibody dynamics approach

Design of an Efficient Climbing Flight Trajectory for a Flapping-Wing Micro Air Vehicle

Smart material systems for vibration monitoring and suppression

Integrated framework for jitter analysis combining disturbance, structure, vibration isolator and optical model

Design and prototyping of rotational Bi-stable mechanism using permanent magnets

Design of a deployable solar concentrator using Fresnel lenses for space-based solar power applications

Mode Selection in Component Mode Synthesis via Displacement-Based Partitioned Equations

An aeroelastic analysis of a flexible flapping wing using modified strip theory

An aerodynamic model for insect flapping wings in forward flight

Design and construction of pre-stressed piezoelectric unimorph for trailing edge flap actuation

Aeroelastic analysis of airfoils at proximity with structural coupling

Experimental investigation on the aerodynamic characteristics of a bio-mimetic flapping wing with macro-fiber composites

Performance Evaluation of Hybrid Vibration Isolator using FxLMS algorithm

Tachi-Miura Polyhedron 실린더 구조에서의 비선형 탄성파 전파 특성에 관한 연구

SNAP-THROUGH MOTION ESTIMATION OF A BUCKLED BISTABLE COMPOSITE BEAM

Aerodynamic effects of deviating motion of flapping wings in hovering flight

Dynamic characteristics of ER fluid-filled composite plate using multielectrode configuration

Study on a spin stabilization technique using a spin table

Design of three parameter isolator for the RWA disturbance considering flexible structural effects

Shock response prediction of a low altitude earth observation satellite during launch vehicle separation

Electroactive behavior of poly (acrylic acid) grafted poly (vinyl alcohol), their synthesis by Ce (IV) glucose redox system and characterization

Effect of body aerodynamics on the dynamic flight stability of the hawkmoth Manduca sexta

Optimal Hovering Wing Kinematics of Flapping-Wing Model Using Reinforcement Learning

Nonlinear finite element simulation of shape adaptive structures with SMA strip actuator

Leading-edge curvature effect on flapping performance of low aspect ratio wings in forward flight

Dynamic stability of flapping-wing micro air vehicles with unsteady aerodynamic model

Active Vibration Isolation System Using the Piezoelectric Unimorph With Mechanically Pre-Stressed Substrate

Ornithopter modeling for flight simulation

'DEVELOPMENT OF A SERVO-DRIVEN FLAPPING-WING AIR VEHICLE WITH FOLDING-WING MECHANISM

Parametric investigation on plasma streamwise vortex generators with flow around the bluff body

Mathematical Simulation of Combustion Experiments with Dynamic Volume Considering the Internal Condition of Combustion Chamber

Limit-cycle oscillation suppression of bioinspired ornithopter: wind tunnel testing

Study of flapping actuator modules using IPMC

Compressed mesh washer isolators using the pseudoelasticity of SMA for pyroshock attenuation

Camber-adjustable flapping wing air vehicles

Blade deformation measurement of a model-scale rotor system using a SPR system with IR cameras

Effective elastic, thermoelastic, and piezoelectric properties of braided composites using equivalent laminate modeling

Performance Evaluation of RWA Vibration Isolator Using Notch Filter Control

Online phase tracking of interferometric optical fiber sensors for vibration control

Teaching a micro air vehicle how to fly as we teach babies how to walk

Indoor flight testing and controller design of bioinspired ornithopter

Development of a point tracking system for measuring structural deformations using commercial video cameras

Optimal design of a flexible flapping wing using fluid-structure interaction analysis

Control of tailed flapping-wing flying robot

Experimental study on the flight dynamics of a bioinspired ornithopter: free flight testing and wind tunnel testing

Wind tunnel tests for a flapping wing model with a changeable camber using macro-fibercomposite actuators

Aeroelastic Analysis of Wind Turbine Blades using Modified Strip Theory

Performance Evaluation for Piezoelectric Unimorph Actuator with Stress Distribution

Development of multi-DOF active microvibration emulator

Parameter optimization of foldable flapping-wing mechanism for maximum lift

Unsteady aerodynamic characteristics of the oscillating airfoil using MSBs

Evaluation of Piezoelectric Nonlinear Properties According to Internal Stresses and Applied Electric Fields

Dynamic Modeling of Scissors Structure and Stiffness Analysis Based on Deployed Configuration

Numerical prediction of permeability and effective thermal conductivity in simple cubic and body-centered truss structures

Effects of sweep-motion profile on rigid and flexible flapping-wing aerodynamics

An improved quasi-steady aerodynamic model for insect wings that considers movement of the center of pressure

Effects of advance ratio on the aerodynamic characteristics of an insect wing in forward flight

Pyroshock and Vibration Attenuation Tests using Compressed Mesh Washer Isolators with the Application of Pseudoelastic SMA Wire

MSBS-SPR integrated system allowing wider controllable range for effective wind tunnel test

Periodic tail motion linked to wing motion affects the longitudinal stability of ornithopter flight

Experimental evaluation of a flapping-wing aerodynamic model for MAV applications

Analytical & Experimental Study on Microvibration Effects of Satellite

Fabrication and electromagnetic characteristics of microwave absorbers containing carbon nanofibers and magnetic metals

Development of a real-time point tracker system for MAV wind tunnel tests using commercial video cameras

Fabrication and electromagnetic characteristics of electromagnetic wave absorbing sandwich structures

Estimation of dynamic structural displacements using fiber Bragg grating strain sensors

Optimal placement of piezoelectric sensors and actuators for vibration control of a composite plate using genetic algorithms

Displacement field estimation for a two-dimensional structure using fiber Bragg grating sensors

Postbuckling and vibration characteristics of piezolaminated composite plate subject to thermo-piezoelectric loads

An experimental study of active vibration control of composite structures with a piezo-ceramic actuator and a piezo-film sensor

Fabrication and electromagnetic characteristics of microwave absorbers containing carbon nanofibers and NiFe particles

Shape estimation with distributed fiber Bragg grating sensors for rotating structures

Application of MWNT-added glass fabric/epoxy composites to electromagnetic wave shielding enclosures

Analysis of composite plates with piezoelectric actuators for vibration control using layerwise displacement theory

Microwave absorbing hybrid composites containing Ni–Fe coated carbon nanofibers prepared by electroless plating

Multi-modal vibration control using adaptive positive position feedback

Extended unsteady vortex-lattice method for insect flapping wings

Erratum to: Ornithopter flight simulation based on flexible multi-body dynamics

Ornithopter flight simulation based on flexible multi-body dynamics

Aeroelastic characteristics of cylindrical hybrid composite panels with viscoelastic damping treatments

Thermal post-buckling analysis of shape memory alloy hybrid composite shell panels

Space Structures and H/W Systems Lab

교수님 소개

한재흥

연구실 소개

연구실 키워드

알럼나이가 간 회사

연구실 지원 방법

대우 조건

연도별 논문 인용수

저널 & 학회 논문 출판 수

연구실 논문 목록

Multidisciplinary design optimization of the flapping-wing air vehicle using artificial neural network surrogate model

Design of a deployable solar concentrator using Fresnel lenses for space-based solar power applications

Mode Selection in Component Mode Synthesis via Displacement-Based Partitioned Equations

연구실 보유 특허

대학별 입시끈

우리 연구실 모집

교수님 소개

한재흥

연구실 키워드

알럼나이가 간 회사

연구실 지원 방법

대우 조건

연도별 논문 인용수

저널 & 학회 논문 출판 수

연구실 논문 목록

Multidisciplinary design optimization of the flapping-wing air vehicle using artificial neural network surrogate model

Design of a deployable solar concentrator using Fresnel lenses for space-based solar power applications

Mode Selection in Component Mode Synthesis via Displacement-Based Partitioned Equations

연구실 보유 특허

최근 3년간 연구실적 높은 연구실

대학별 입시끈

우리 연구실 모집