• 한국항공우주학회지
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• 제49권7호
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• pp.549-555
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• 2021

원공이 있는 복합재 적층판의 강도는 복합재 항공기기 설계 시 충격하중이 가해지는 부위의 설계 허용치로 사용된다. 일반적으로 BVID (Barely Visible Impact Damage)에 의한 강도저하는 24.0 mm 폭의 시편에 6.0 mm 지름의 원공이 있는 시편의 강도로 가정한다. 본 연구에서는 원공이 있는 복합재 적층판의 강도에 적층각이 미치는 영향을 조사하기 위해 잔류강도 시험을 수행하였다. 원공이 있는 적층판의 강도를 예측하기 위해 특성길이를 이용한 점응력 파손기준을 사용하였고, 이론해를 검증하기 위하여 유한요소해석을 수행하였다. 실험결과로부터 특성길이는 0°, ±45°와 90°층의 비율과 관련이 있음을 보였다. 또한 회귀분석을 통하여 임의의 적층 패턴에 대한 특성길이와 원공이 없는 시편의 강도를 결정하였다.

• 한국항공우주학회지
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• 제38권10호
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• pp.1020-1025
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• 2010

탑재 교정용 흑체는 우주용 영상센서의 시간경과 및 재 구동에 따른 센서의 특성변화 교정을 통한 영상품질향상을 위해 적용된다. 본 논문에서 제안한 영상센서의 비균일 특성 교정을 위한 흑체 열설계는 저온에서 고온에 이르는 흑체의 온도정보 제공을 위한 흑체 가열용 히터, 흑체 가열 후 잔열 수송 및 심해우주로의 열 방출을 위한 히트파이프와 방열판 그리고 비교정임무 수행동안 흑체가 특정온도를 유지하며 원하는 시점에서 언제든지 교정임무 수행이 가능하도록 하는 방열판용 히터로 구성된다. 흑체 열설계에 대한 타당성을 궤도 열해석을 통해 입증하였다.

• Structural Engineering and Mechanics
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• 제50권4호
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• pp.525-539
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• 2014

Bonded composite-patch repair has been widely used to restore or extend the service life of damaged structures due to its effectiveness as a mechanical repair technique. In this paper using extended finite element method (XFEM), three-dimensional crack models are developed to examine the fracture behavior of centrally cracked aluminum plates repaired with single and double sided composite patches. Stress intensity factor (SIF) at the crack tip is used as the fracture criterion. In this regard, the effects of the crack lengths, patch materials, orientation of plies, adhesive and patch thickness are examined to estimate the SIF of the repaired plate and the repair performance. The obtained results show that composite patches have significant effect on reduction of the SIF at the crack tip. It is also proved that using double symmetric repair, in comparison to single one, reduces considerably SIF at the crack tip. Hence, the residual strength can be improved significantly as well as fatigue life of the structure. Investigation of ply orientation effects shows SIF increase as the ply orientation is changed from $0^{\circ}$ (perpendicular to the advancing crack) to $90^{\circ}$ (parallel to the crack line). However, the effectiveness of the ply orientation depends on the loading direction and the crack direction.

• Structural Engineering and Mechanics
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• 제55권1호
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• pp.229-244
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• 2015

H-infinity norm relates to the maximum in the frequency response function and H-infinity control method focuses on the case that the vibration is excited at the fundamental frequency, while 2-norm relates to the output energy of systems with the input of pulses or white noises and 2-norm control method weighs the overall vibration performance of systems. The trade-off between the performance in frequency-domain and that in time-domain may be achieved by integrating two indices in the mixed vibration control method. Based on the linear fractional state space representation in the modal space for a piezoelectric flexible structure with uncertain modal parameters and un-modeled residual high-frequency modes, a mixed dynamic output feedback control design method is proposed to suppress the structural vibration. Using the linear matrix inequality (LMI) technique, the initial populations are generated by the designing of robust control laws with different H-infinity performance indices before the robust 2-norm performance index of the closed-loop system is included in the fitness function of optimization. A flexible beam structure with a piezoelectric sensor and a piezoelectric actuator are used as the subject for numerical studies. Compared with the velocity feedback control method, the numerical simulation results show the effectiveness of the proposed method.

• Journal of Biosystems Engineering
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• 제30권5호
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• pp.268-273
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• 2005

This study was conducted to investigate the specificities of four fulcrum types for geo-statistical analysis of elevation within rice paddy field. In Korea, the spaces between inter-rows and between hills for rice transplanting are 30cm and 11cm to 14cm, respectively. So, the size and shape of fulcrum for field elevation measurement should be considered according to the inter-row and the hill spaces. Four kinds of fulcrum were chosen such as round-shape with 2.5cm diameter, circular-shape with 10cm diameter, 10cm (one third of inter-row space) by 24cm (double of hill space) rectangular-shape, and 20cm (two-thirds of inter-row space) by 24cm rectangular-shape. The resulting descriptive statistics couldn't determine the best fulcrum type to measure the rice paddy field elevation. But the results of geo-statistical analysis could determine the best fulcrum type. In the case of 10cm by 24cm rectangular-shape fulcrum, Nugget and range, meaning measurement error and/or noise, and limit of spatial connection, respectively, were minimum; Q value meaning weight of spatial structure and $r^2$ value were minimum, and residual sum of squares was minimum. It means that 10cm by 24 cm rectangular-shape fulcrum could best describe the rice paddy field elevation.

• Journal of Electrical Engineering and Technology
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• 제6권5호
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• pp.697-705
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• 2011

In this paper, a closed-loop system constructed with a linear plant and nonlinearity in the feedback connection is considered to argue against its planar orbital stability. Through a state space approach, a main result that presents a sufficient stability criterion of the limit cycle predicted by solving the harmonic balance equation is given. Preliminarily, the harmonic balance of the nonlinear feedback loop is assumed to have a solution that determines the characteristics of the limit cycle. Using a state-space approach, the nonlinear loop equation is reformulated into a linear perturbed model through the introduction of a residual operator. By considering a series of transformations, such as a modified eigenstructure decomposition, periodic averaging, change of variables, and coordinate transformation, the stability of the limit cycle can be simply tested via a scalar function and matrix. Finally, the stability criterion is addressed by constructing a composite Lyapunov function of the transformed system.

• Current Optics and Photonics
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• 제2권6호
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• pp.612-622
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• 2018

In wave-front-sensor-less adaptive optics (WFS-less AO) systems, the Jacopo Antonello (JA) method belongs to the model-based class and requires few iterations to achieve acceptable distortion correction. However, this method needs a lot of measurements, especially when it deals with moderate or severe aberration, which is undesired in free-space optical communication (FSOC). On the contrary, the stochastic parallel gradient descent (SPGD) algorithm only requires three time measurements in each iteration, and is widely applied in WFS-less AO systems, even though plenty of iterations are necessary. For better and faster compensation, we propose a WFS-less hybrid approach, borrowing from the JA method to compensate for low-order wave front and from the SPGD algorithm to compensate for residual low-order wave front and high-order wave front. The correction results for this proposed method are provided by simulations to show its superior performance, through comparison of both the Strehl ratio and the convergence speed of the WFS-less hybrid approach to those of the JA method and SPGD algorithm.

• 한국항공우주학회지
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• 제45권10호
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• pp.881-891
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• 2017

본 논문에서는 인공위성의 궤도예측을 위해 사용되는 미국 합동우주관제센터(JSpOC, Joint Space Operation Center)의 TLE(Two Line Element) 정보에 대한 SGP4(Simplified General Perturbations 4) 모델의 장기 궤도예측 오차를 줄이기 위해 과거의 TLE 정보들을 이용한 보상기법을 적용하여 새로운 TLE 정보를 생성하는 방법에 대해 기술하고 있다. 이를 위해 과거 특정 시점에서의 TLE 정보를 바탕으로 현재까지 궤도전파를 한 데이터와 동일기간 동안 미국 합동우주관제센터에서 공개된 모든 TLE를 이용해서 궤도전파를 수행한 데이터를 비교하여 계산한 궤도잔차를 이용하였다. 이러한 궤도잔차 성분은 SGP4 궤도전파 모델에 의한 궤도오차 증가 경향을 보여주고 있기 때문에 궤도오차 보정을 위해 해당 궤도잔차 성분들을 적절한 함수로 표현하였다. 이후, 현재 시점에서 공개된 TLE 정보를 이용한 SGP4 궤도전파 데이터에 해당 잔차함수를 적용함으로써 장기 궤도전파에 따른 SGP4 모델의 궤도오차를 줄일 수 있었으며, 이를 바탕으로 새로운 TLE 정보를 생성하였다. 본 논문에서 일주일의 궤도전파에 대한 시뮬레이션을 통해 기존의 TLE를 이용한 궤도전파 오차가 4km 정도인 반면 새로운 TLE 생성기법에 의한 궤도전파 오차가 약 2km 수준으로 줄어드는 것을 확인할 수 있었다.

• Structural Engineering and Mechanics
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• 제61권6호
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• pp.701-709
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• 2017

Seismic dissipation devices can play a crucial role in mitigating earthquake damages, loss of life and post-event repair and downtime costs. This research investigates the use of ring springs with high-force-to-volume (HF2V) dissipaters to create damage-free, recentring connections and structures. HF2V devices are passive rate-dependent extrusion-based devices with high energy absorption characteristics. Ring springs are passive energy dissipation devices with high self-centring capability to reduce the residual displacements. Dynamic behaviour of a system with nonlinear structural stiffness and supplemental hybrid damping via HF2V devices and ring spring dampers is used to investigate the design space and potential. HF2V devices are modelled with design forces equal to 5% and 10% of seismic weight and ring springs are modelled with loading stiffness values of 20% and 40% of initial structural stiffness and respective unloading stiffness of 7% and 14% of structural stiffness (equivalent to 35% of their loading stiffness). Using a suite of 20 design level earthquake ground motions, nonlinear response spectra for 8 different configurations are generated. Results show up to 50% reduction in peak displacements and greater than 80% reduction in residual displacements of augmented structure compared to the baseline structure. These gains come at a cost of a significant rise in the base shear values up to 200% mainly as a result of the force contributed by the supplemental devices.

• 한국결정성장학회지
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• 제7권2호
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• pp.244-252
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• 1997

$LiCO_3, Al_2O_3, Fe_2O_3$ 혼합물을 1620K에서 반응시켜 리튬전지의 음극재료로 응용이 가능한 스핀넬형 $LiAl_{2.5}/Fe_{2.5}O_8$를 합성하였다. XRD의 Rietveld 해석을 통하여 결정구조 해석을 하였다. 고용체의 공간군은 $P4_3$32(a=8.1293$\AA$)이고, 결정구조해석의 최종 Residual index는 약 5%정도이었다. 역 스핀넬구조에서 양이온 $Al^{3+}, Fe^{3+}$은 4-배위와 6-배위로 위치하고, $Li^+$은 4b, 12d의 6-배위자리에 존재하였다.