• Advances in aircraft and spacecraft science
• /
• 제5권3호
• /
• pp.335-348
• /
• 2018

The structural dynamics (SD) behavior of Elastic Flapping Wings (EFWs) is investigated analytically as a novel approach in EFWs analysis. In this regard an analytical SD solution of EFW undergoing a prescribed rigid body motion is initially derived, where the governing equations are expressed in modal space. The inertial forces are also analytically computed utilizing the actuator induced acceleration effects on the wing structure, while due to importance of analytical solution the linearity assumption is also considered. The formulated initial-value problem is solved analytically to study the EFW structural responses, where the effect of structure-actuator frequency ratio, structure-flapping frequency ratio as well as the structure damping ratio on the EFW pick amplitude is analyzed. A case study is also simulated in which the wing is modeled as an elastic beam with shell elements undergoing a prescribed sinusoidal motion. The corresponding EFW transient and steady response in on-off servo behavior is investigated. This study provides a conceptual understanding for the overall EFW SD behavior in the presence of inertial forces plus the servo dynamics effects. In addition to the substantial analytical results, the study paves a new mathematical way to better understanding the complex role of SD in dynamic EFWs behavior. Specifically, similar mathematical formulations can be carried out to investigate the effect of aerodynamics and/or gravity.

• Korea-Australia Rheology Journal
• /
• 제16권3호
• /
• pp.117-128
• /
• 2004

The effect of molecular parameters on the steady vortex behaviors in the inertial viscoelastic flow past a cylinder has been investigated. FENE-CR model was considered as a constitutive equation. A recently developed iterative solution method (Kim et al., (in press)) was found to be successfully applicable to the computation of inertial viscoelastic flows. The high-resolution computations were carried out to understand the detailed flow behaviors based on the efficient iterative solution method armed with ILU(0) type pre-conditioner and BiCGSTAB method. The discrete elastic viscous split stress-G/streamline upwind Petrov Galerkin (DEVSS-G/SUPG) formulation was adopted as a stabilization method. The vortex size decreased as elasticity increases. However, the vortex enhancement was also observed in the case of large extensibility, which means that the vortex behavior is strongly dependent upon the material parameters. The longitudinal gradient of normal stress was found to retard the formation of vortex, whereas the extensional viscosity played a role in the vortex enhancement. The present results are expected to be helpful for understanding the inertial vortex dynamics of viscoelastic fluids in the flow past a confined cylinder.

• 제어로봇시스템학회:학술대회논문집
• /
• 제어로봇시스템학회 2001년도 ICCAS
• /
• pp.32.5-32
• /
• 2001

There has been many teleoperation systems handling the micro object. However, the stability problem for these systems has not been mentioned yet. Historically, Lawrence[1] proposed the Transparency-Optimized Architecture and passivity theorem for stability analysis of bilateral teleoperation. He claimed that unless the task(or environment) impedance contains significance inertial behavior, Passivity condition for Transparency-optimized architecture is not satisfied. In this paper we propose one method which satisfies passivity condition for the micro-teleoperation system handling a insignificant inertial object and is based on the structure of Lawrence and Hashtrudi-Zaad[2] and velocity-force scaling.

• 한국지반공학회논문집
• /
• 제29권4호
• /
• pp.33-44
• /
• 2013

Mononobe-Okabe (M-O) 이론은 현재 국내외에서 가장 일반적으로 사용되는 지진 시 옹벽에 작용하는 동적토압 산정 방법이다. M-O방법은 강체거동(Rigid Behavior)을 갖는 중력식 옹벽의 사질토 뒤채움 지반에 대하여 제안된 방식이지만 현재 여러 지반 조건 및 캔틸레버 형태의 옹벽에도 널리 적용되고 있다. M-O 방법은 지진 시 발생하는 뒤채움 지반의 관성력만을 고려하기 때문에 벽체의 관성력이 동적 토압에 미치는 영향을 고려하지 못하는 단점이 있다. 본 논문에서는 M-O 방법을 포함하여 지진 시 옹벽에 작용하는 동적토압을 산정하는 기존에 제안된 방법들의 이론적 배경 및 현재까지의 연구동향을 분석하였으며, 이를 통하여 지진 시 토압산정의 중요한 요소인 동적토압의 분포 및 작용점에 대한 합리적인 재평가가 필요함을 도출하였다. 역 T형 옹벽을 대상으로 동적원심모형실험을 수행하여 지진 시 옹벽에 작용하는 동적 토압을 M-O 이론과 모형 모델 거동과의 비교를 통하여 차이점을 평가하였다. 실험 결과, 지진 시 옹벽의 실제 거동은 M-O 방법의 가정과 달리 벽체의 관성력과 동적토압 사이에 위상차가 발생함을 알 수 있었다. 또한 벽체에서 주동방향으로 최대 휨 모멘트 발생 시 계측된 토압은 정적토압보다 감소하는 결과를 보였으며 이는 벽체 관성력이 원인인 것으로 판단된다.

• 제어로봇시스템학회:학술대회논문집
• /
• 제어로봇시스템학회 2001년도 ICCAS
• /
• pp.167.4-167
• /
• 2001

Accurate mathematical models of spacecraft components are an essential of spacecraft attitude control system design, analysis and simulation. Gyro is one of the most important spacecraft components used for attitude propagation and control. Gyro errors may seriously degrade the accuracy of the calculated spacecraft angular rate and of attitude estimates due to inherent drift and bias errors. In this paper, a detailed mathematical model of gyro containing the relationships for predicting spacecraft angular rate and disturbances is proposed. Stochastic model describing random drift behavior is discussed in frequency domain and time domain. In order to illustrate this approach, we analyze the behavior for Litton´s Space Inertial Reference Uint(SIRU).

• 한국강구조학회 논문집
• /
• 제14권6호
• /
• pp.701-710
• /
• 2002

본 연구에서는 개단면 리브를 갖는 보강판이 직교이방성 특성을 고려한 직교이방성 판 요소 프로그램을 개발하고, 여러가지 보강판에 대한 민감도 분석 및 매개변수 연구를 통하여 보강판의 직교이방성 거동 특성 및 본 프로그램의 적용성을 살펴보았다. 먼저 보강재만의 관성 모멘트를 강판만의 관성 모멘트로 나눈 값을 관성 모멘트 비라 정의하고, 여러가지 보강판에 대한 민감도 분석을 실시하였다. 보강판의 직교이방성 거동을 규명하였다. 본 프로그램의 적용성을 살펴보기 위하여, 여러가지 보강판에 대한 매개변수 연구를 수행하고, 최대 처짐에 대한 결과를 등팡성 판 요소를 이용한 ABAQUS의 결과와 비교하였다. 비교 결과, 두 결과가 잘 일치하는 특정 모멘트 비를 직교이방성 판으로 해석할 수 있는 기준으로 제안하였으며, 두 결과 사이의 오차율을 관성 모멘트 비의 함수 식으로 표현하였다. 따라서, 개단면 리브로 보강된 판을 직교이방성 판으로 해석하기 위해서는 제안한 특정 관성 모멘트 비 이상의 값을 가져야 안전측의 결과를 얻으며, 또한 본 연구에서 제안한 상관 함수를 이용하여 결과를 보정하면 간편하게 타당한 결과를 얻을 수 있을 것으로 사료된다.

• Geomechanics and Engineering
• /
• 제34권6호
• /
• pp.649-664
• /
• 2023

Structural inertial interaction is a representative the effect of dynamic soil-foundation-structure interaction (SFSI), which leads to a relative displacement between soil and foundation, period lengthening, and damping increasing phenomena. However, for a system with a significantly heavy foundation, the dynamic inertia of the foundation influences and interacts with the structural seismic response. The structure-to-foundation mass ratio (MR) quantifies the distribution of mass between the structure and foundation for a structure on a shallow foundation. Although both systems exhibit the same vertical factor of safety (FS_v), the MR and corresponding seismic responses attributed to the structure and foundation masses may differ. This study explored the influence of MR on the permanent deformation and seismic response of soil-foundation-structure system considering SFSI via numerical simulations. Given that numerous dimensionless parameters of SFSI described its influence on the structural seismic response, the parameters, except for MR and FS_v, were fixed for the sensitivity analysis. The results demonstrated that the foundation inertia of heavier foundations induced more settlement due to sliding behavior of heavily-loaded systems. Moreover, the structural inertia of heavier structures evidently exhibited foundation rocking behavior, which results in a more elongated natural period of the structure for lightly-loaded systems.

• 스마트미디어저널
• /
• 제13권5호
• /
• pp.19-25
• /
• 2024

발달장애인의 사회 진입을 막는 가장 큰 행동 유형은 공격 행동이다. 공격 행동은 발달장애인 자신의 안전뿐만 아니라 타인의 신체적 안전에도 위협이 될 수 있다. 본 연구에서는 저전력 프로세서를 활용한 웨어러블 시스템을 제안한다. 제안된 시스템은 IMU(Inertial Measurement Unit, 관성 측정 장치)가 적용되어, 사용자의 행동을 분석할 수 있으며, 개발된 시스템에 부착된 LED 배열을 통해 일정 시간 이상 공격 행동이 감지되지 않을 시, 흥미로운 LED 패턴을 표현하여 발달장애인에게 보상을 통한 행동 중재를 제공한다. 전원이 제한된 환경에서 장시간 착용해야 하는 시스템을 구현하기 위해 데이터의 전처리 과정부터 AI 모델 적용까지 전 단계에 걸쳐서 성능-에너지 소모 간 최적화 방법을 제시한다.

• Advances in aircraft and spacecraft science
• /
• 제7권1호
• /
• pp.1-17
• /
• 2020

In this paper, a new model-based Fault Detection and Diagnosis (FDD) method for an agile supersonic flight vehicle is presented. A nonlinear model, controlled by a classical closed loop controller and proportional navigation guidance in interception scenario, describes the behavior of the vehicle. The proposed FDD method employs the Inertial Navigation System (INS) data and nonlinear dynamic model of the vehicle to inform fins damage to the controller before leading to an undesired performance or mission failure. Broken, burnt, unactuated or not opened control surfaces cause a drastic change in aerodynamic coefficients and consequently in the dynamic model. Therefore, in addition to the changes in the control forces and moments, system dynamics will change too, leading to the failure detection process being encountered with difficulty. To this purpose, an equivalent aerodynamic model is proposed to express the dynamics of the vehicle, and the health of each fin is monitored by the value of a parameter which is estimated using an adaptive robust filter. The proposed method detects and isolates fins damages in a few seconds with good accuracy.

• Structural Engineering and Mechanics
• /
• 제83권1호
• /
• pp.1-17
• /
• 2022

The static design approach in the current code implies that the inherent torsional moment represents the state of zero inertial torsional moments at the center of mass (CM). However, both experimental and analytical results prove the existence of a large amount of the inertial torsional moment at the CM. Also, the definition of eccentricity by engineers, which is referred to as the resistance eccentricity, is defined as the distance between the center of mass and the center of resistance, which is conceptually different from the static eccentricity in the current codes, defined as the arm length about the center of rotation. The difference in the definitions of eccentricity should be made clear to avoid confusion about the torsion design. This study proposed prediction equations as a function of resistance eccentricity based on a resistance eccentricity model with advantages of (1) the recognition of the existence of torsional moment at the CM, (2) the avoidance of the confusion by using resistance eccentricity instead of the design eccentricity, and (3) a clear relationship of applied inertial forces at the CM and resisting forces. These predictions are compared with the seismic responses obtained from time-history analyses of a five-story building structure under moderate and severe earthquakes. Then, the trend of the resistance eccentricity corresponding to the maximum edge drift is investigated for elastic and inelastic responses. The comparison given in this study shows that these prediction equations can serve as a useful reference for the prediction in both the elastic and the inelastic ranges.