• 한국항공우주학회지
• /
• 제46권9호
• /
• pp.752-759
• /
• 2018

본 논문에서는 비선형 모델 시뮬레이션을 통해 저속 회전 중인 유도포탄의 비행 모습을 확인하고 외란으로써 여러 가지 방향과 크기의 돌풍을 작용하여 유도포탄의 비행 안정성을 분석한 방법과 결과를 소개한다. 돌풍은 3m/s, 7m/s, 10m/s, 15m/s 네 가지의 속력을 가지고 26가지의 방향에서 탄도 정점 부근부터 작용하도록 설정하였다. 초당 1회전 및 3회전으로 회전하는 경우에 대해 총 208회의 시뮬레이션을 수행한 결과를 분석하였다. 초당 3회전으로 회전할 때는 탄체가 전복되지 않았지만, 초당 1회전으로 회전할 때는 7m/s 이상의 돌풍이 작용할 때 비행 후반부에 탄체가 전복되는 경우가 발견되었다. 탄체 비행 방향 반대쪽으로 작용하여 비행 방향 대기속도를 증가하는 돌풍은 해로운 영향을 주지 않았다. 탄체 전복은 모두 탄체가 하강하는 후반부에 발생하였으며, 탄도 정점 부근에서는 자세가 크게 진동하거나 탄체가 전복되지 않았다.

• Investigative Magnetic Resonance Imaging
• /
• 제5권2호
• /
• pp.116-122
• /
• 2001

목적 : 고식적 스핀에코, 위상 대조 경사에코, 고속 GRASS, 중T-2강조 고속스핀에코 연쇄를 각각 유동모형에 적용시켜, 저속유동에 대한 자기공명영상의 민감도를 찾아내고자 한다. 대상 및 방법 뇌실-복강 단락 도관과 GE 모형으로 이루어진 유동모형으로 싸이폰 효과에 의한 지속적인 가변 유속의 흐름을 내보내고, 각각의 유속에 위의 네 가지 자기공명영상연쇄를 적용시켰다. 0.08 ml/min 에서 1.7 ml/min 범위의 유량의 흐르는 액체와 정지된 액체에서 획득된 자기공명영상의 신호강도를 비교한 결과를 요약하면 다음과 같다. 결과 0.17 ml/min 이상의 느린 흐름에서는 고식적 스핀에코영상이 가장 우수한 정지-유동 액체사이의 겉보기대조를 보이나, 그 이하의 매우 느린 흐름에서는 GRASS 영상이 더 높은 민감도를 보였다. 결론 : 4가지 자기공명펄스연쇄는 0.08 ml/min에서 1.7 ml/min 범위의 유량의 흐름에서 서로 다른 민감도를 보였다. 이 결과는 임상적으로, 단락수술후의 뇌척수액의 흐름이나 혈관내의 혈전에 의한 흐름의 변이 등의 인체내의 저속유동을 검출하는 비침습적방법으로 유용하게 적용될 수 있을 것이다.

• 천문학회보
• /
• 제43권1호
• /
• pp.33.1-33.1
• /
• 2018

The differential rotational properties of early-type galaxies (ETGs) revealed by integral field spectroscopy surveys is arguably one of the most exciting findings in the galaxy evolution study during the past decade. Numerical studies have shown that galaxy mergers under various configurations can reproduce the observed distribution of ETG spin. However, we suggest an alternative scenario for the spin evolution of a large fraction of ETGs. Using the Horizon-AGN simulation, we follow the spin evolution of 10037 color-selected ETGs more massive than 1010 Msun that are divided into four groups: cluster centrals (3%), cluster satellites (33%), group centrals(5%), and field ETGs (59%). We find a strong mass dependence of the slow rotator fraction, fSR, and the mean spin of massive ETGs. Although the environmental dependence is not clear in the fSR, it is visible in the mean value of the spin parameter. The environmental dependence is driven by the satellite ETGs whose spin gradually decreases as their environment becomes denser. Galaxy mergers appear to be the main cause of total spin changes in 94% of central ETGs of halos with Mvir > 1012.5 Msun, but only 22% of satellite and field ETGs. We find that non-merger induced tidal perturbations better correlate with the galaxy spin-down in satellite ETGs than mergers. Given that the majority of ETGs are not central in dense environments, we conclude that non-merger tidal perturbation effects played a key role in the spin evolution of ETGs observed in the local (z < 1) universe.

• 유체기계공업학회:학술대회논문집
• /
• 유체기계공업학회 2006년 제4회 한국유체공학학술대회 논문집
• /
• pp.323-326
• /
• 2006

Numerical solutions for spin-up problem of a thermally stratified fluid in a cylinder with an insulating sidewall and time-dependent rotation rate are presented. Detailed results are given for aspect ratio of O(1), fixed Ekman number $10-^{4}$, Rossby number 0.05 and Prandtl number O(1). Angular velocity of a cylinder wall changes with following formula, $\Omega_f=\Omega_i+\Delta\Omega[1-\exp(-t/t_c)]$. Here, this $t_c$, value, which is very significant in present study, represents that how fast/slow the angular velocity of the cylinder wall reaches final angular velocity. The normalized azimuthal velocity and meridional flow plots for several tc value which cover ranges of the stratification parameter S(1 ~ 10) are presented. The role of viscous-diffusion and Coriolis term in present study is examined by diagnostic analysis of the azimuthal velocity equation.

• 천문학회지
• /
• 제45권2호
• /
• pp.49-57
• /
• 2012

In this study, I calculate the past and future dynamical states of the Earth-Moon system by using modified Lambeck's formulae. I find that the ocean tidal effect must have been smaller in the past compared to its present amount. Even though the Moon is already in the spin-orbit synchronous rotational state, my calculation suggest that it will not be in geostationary rotational state in the next billion years or so. This is due to the associated Earth's obliquity increase and slow retardation of Earth's spin and lunar orbital angular velocities. I also attempt to calculate the precessional period of the Earth in the future. To avoid uncertainties in the time scale, the future state is described by using the Earth-Moon distance ratio as independent parameter. Effects due to solar tidal dissipation are included in all calculations.

• Advances in aircraft and spacecraft science
• /
• 제9권5호
• /
• pp.449-462
• /
• 2022

Space-telescopes placed in the Sun-Earth second Lagrange point (L2) observe the sky following a scan strategy that is usually based on a spin-precession motion. Knowing which regions of the sky will be more observed by the instrument is important for the science operations and the instrument calibration. Computing sky observation parameters numerically (discretizing time and the sky) can consume large amounts of time and computational resources, especially when high resolution isrequired.This problem becomesmore critical if quantities are evaluated at detector level instead of considering the instrument entire Field of View (FoV). In previous studies, the authors have derived analytic solutions for quantities that characterize the observation of each point in the sky in terms of observation time according to the scan strategy parameters and the instrument FoV. Analytic solutions allow to obtain results faster than using numerical methods as well as capture detailed characteristics which can be overseen due to discretization limitations. The original approach is based on the analytic expression of the instrument trace over the sky. Such equations are implicit and thusrequiresthe use of numeric solversto compute the quantities.In this work, a new and simpler approach for computing one ofsuch quantities(mean observation time) is presented.The quantity is first computed for pure spin motion and then the effect of the spin axis precession is incorporated under the assumption that the precession motion is slow compared to the spin motion.In this sense, this new approach further simplifies the analytic approach, sparing the use of numeric solvers, which reduces the complexity of the implementation and the computing time.

• 대한전기학회논문지:시스템및제어부문D
• /
• 제49권8호
• /
• pp.459-466
• /
• 2000

In this paper, we propose an attitude controller for an unstructured object using CMG(Control Moment of Gyro) subsystem, which has a stabilizer function. The CMG subsystem consists of one motor for spinning the wheel and the other motor for turning the outer gimbal. While the wheel of CMG subsystem is spinning at high speed, applying force to the spin axis of the wheel leads the torque about the vertical axis. We utilize the torque to control the attitude of object in this study. For the stabilizer function, in additiion, holding the load at the current position, the power applied to the gimbal motor of CMG will be cut, which result in the braking force to stop the load by gyro effect. However, due to the gear reduction connected to outer gimbal, slow load motion cannot generate the braking force. Thus, in this study, we are willing to make a holding force by applying control power to the gimbal motor from the signal of piezoelectric gyroscopic sensor that detected the angular velocity of the load. These two features are demonstrated in experiment, carrying a beam with crane. As a result, load was started to rotate by controlling gimbal positiion and was stopped by turning off the gimbal power. Moreover, slow movement of the load was also rejected by additional control with gyroscopic sensor.

• 한국항공우주학회지
• /
• 제48권9호
• /
• pp.681-689
• /
• 2020

본 논문에서는 유도형 탄약의 모사 기체를 제작하고 공중에서 탄체에 롤축 회전을 인가한 뒤 롤축 저속 회전 중인 탄체의 롤각 추정 성능을 실험적으로 검증한 방법과 결과를 소개한다. 멀티로터형 무인기를 모선으로 사용해 유도형 탄약 모사 기체에 초기 속도와 고도를 부여하였으며 탄체 투하, 탄체 회전, 롤각 추정 및 안정화로 이어지는 비행 시험 시나리오를 통해 롤각 추정 결과를 분석한다. 약 200m의 고도에서 수평 방향으로 15m/s의 속력으로 탄체를 투하한 뒤 내부의 반동차(Reaction Wheel)를 사용하여 탄체를 회전시켰으며 특히, 상용 GPS/INS와의 비교를 통해 롤각 추정 결과를 제시한다. 아울러, 반동차를 이용하여 공중에서 탄체를 롤축 회전시키는 메커니즘들을 비교하고 실제 구현한 결과도 소개한다.

• Journal of Magnetics
• /
• 제4권3호
• /
• pp.76-79
• /
• 1999

We report results on metastable CuCo ribbons at low Co contents (2 and 10 at %), which were prepared by conventional melt-spinning technique and subsequent annealing. The properties of these materials cannot consistently be described by those of an assembly of superparamagnetic single-domain particles. Magnetic measurements related to magnetic dynamics reveal spin-glass-like properties. Especially, we find very slow nonequilibrium relaxation processes in Co10Cu90, which depend on prehistory, when probing the relaxation of the resistivity. The results are clear evidence for frustrated interaction effects due to magnetic couplings between Co clusters or precipitates in these alloys.

• 한국자기공명학회논문지
• /
• 제23권2호
• /
• pp.40-45
• /
• 2019

The phase transition temperatures and thermodynamic properties of $(NH_4)_2MnCl_4{\cdot}2H_2O$ grown by the slow evaporation method were studied using differential scanning calorimetry and thermogravimetric analysis. A structural phase transition occurred at temperature $T_{C1}$ (=264 K), whereas the changes at $T_{C2}$ (=460 K) and $T_{C3}$ (=475 K) seemed to be chemical changes caused by thermal decomposition. In addition, the chemical shift and the spin-lattice relaxation time $T_{1{\rho}}$ were investigated using $^1H$ magic-angle spinning nuclear magnetic resonance (MAS NMR), in order to understand the role of $NH_4{^+}$ and $H_2O$. The rise in $T_{1{\rho}}$ with temperature was related to variations in the symmetry of the surrounding $H_2O$ and $NH_4{^+}$.