• International Journal of Control, Automation, and Systems
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• 제5권1호
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• pp.93-98
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• 2007

A class of new observers in descriptor linear systems, proportional-derivative(PD) observers, are proposed. A parametric design approach for such observers is proposed based on a complete parametric solution to the generalized Sylvester matrix equation. The approach provides complete parameterizations for all the observer gains, gives the parametric expression for the corresponding left eigenvector matrix of the observer system matrix, realizes elimination of impulsive behaviors, and guarantees the regularity of the observer system.

• 아동학회지
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• 제29권6호
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• pp.87-103
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• 2008

The purpose of this study was to develop an intervention program for decreasing inattentive and impulsive behaviors of children with Attention-Deficit/Hyperactive Disorder (ADHD) by combining cognitive training and cognitive-behavioral therapy. Subjects were 22 children who were classified as ADHD. Eleven children among the 22 were placed randomly in the experimental group; the remaining 11 children were placed in the control group. The effectiveness of the program was analyzed by ANCOVA after controlling for effects of pre-tests on criterion variables. Results of the present study showed that the cognitive intervention program was significantly effective for improving attention span and decreasing impulsivity of children with ADHD.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 1997년도 한국자동제어학술회의논문집; 한국전력공사 서울연수원; 17-18 Oct. 1997
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• pp.1635-1638
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• 1997

A measurement of conduction veloctiy of the action potentials along the muscle fibres has been applied to various diagnosis. When we measure muscle fiber conduction velocity, it occurs that not only change of conduction velocity but alos inclusion of mipulse component by physiological and experimental reason. So, robuster time delay estimation algorithm than general methods[1] is needed to find correct time delay form these signals. In this paper we, propose new time delay estimation algorithms, robust in impulsive noise, by using characteristic of .alpha.-stable distribution whcih defines impulsive noise well. Then we apply proposed algorthms to measure muscle fiber conduction velocity and compare them with other studies.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 1999년도 제14차 학술회의논문집
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• pp.25-28
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• 1999

In this article, a new performance index is proposed to re-duce the collision impulsive force by controlling the null motion of redundant manipulators. First, we define the normalized impact ellipsoid in the viewpoint of instantaneous velocity change. Then, we propose a new impact performance index based on velocity direction for null motion to reduce initial impulsive effects. It gives some advantage for the case of unknown environment. The optimization of this index is that the successional impact forces are reduced. The performance of the proposed index is demonstrated by simulation study.

• Journal of Astronomy and Space Sciences
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• 제38권2호
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• pp.105-117
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• 2021

In this study, a preliminary trajectory design is conducted for a conceptual spacecraft mission to a near-Earth asteroid (NEA) (99942) Apophis, which is expected to pass by Earth merely 32,000 km from the Earth's surface in 2029. This close approach event will provide us with a unique opportunity to study changes induced in asteroids during close approaches to massive bodies, as well as the general properties of NEAs. The conceptual mission is set to arrive at and rendezvous with Apophis in 2028 for an advanced study of the asteroid, and some near-optimal (in terms of fuel consumption) trajectories under this mission architecture are to be investigated using a global optimization algorithm called monotonic basin hopping. It is shown that trajectories with a single swing-by from Venus or Earth, or even simpler ones without gravity assist, are the most feasible. In addition, launch opportunities in 2029 yield another possible strategy of leaving Earth around the 2029 close approach event and simply following the asteroid thereafter, which may be an alternative fuel-efficient option that can be adopted if advanced studies of Apophis are not required.

• 대한수학회논문집
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• 제35권4호
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• pp.1329-1352
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• 2020

In this paper we consider a class of nonlinear evolution equations on infinite dimensional Banach spaces driven by vector measures. We prove existence and uniqueness of solutions and continuous dependence of solutions on the control measures. Using these results we prove existence of optimal controls for Bolza problems. Based on this result we present necessary conditions of optimality.

• Journal of Astronomy and Space Sciences
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• 제26권2호
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• pp.171-186
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• 2009

이 연구에서는 미래 한국의 달 탐사에 대비, 지구-달 천이궤적을 설계하고 분석하였다. 궤적 설계는 최소연료로 지구 주차궤도에서부터 달 임무궤도까지 도달하는 모든 단계에 대해서 실시하였으며 미래 한국의 달 탐사 개발 계획에 실질적인 도움이 되기 위해 2017년, 2020년, 2022년으로 각각 나누어 설계를 하였다. 탐사선의 운동방정식의 구현을 위하여 태양, 지구, 달의 중력에 의한 섭동력이 포함된 N체 운동 방정식을 사용하였으며 보다 실질적인 우주환경의 모사를 위하여 지구의 비대칭 중력장(Geopotential), 태양 복사압(Solar radiation pressure) 그리고 달의 J2 섭동에 의한 영향도 고려하였다. 임무 설계를 위해 가정된 추력은 순간 추력(Impulsive thrust)으로 가정하였으며 발사체의 성능은 현재 개발 예정인 KSLV-2로 가정하였다. 미래 한국의 가상 달 탐사선이 지구-달 천이 궤적(Trans Lunar trajectory)에 진입하는 방법으로는 지구 주차 궤도에서 직접 진입 하는 방법과 여러번의 타원 중개 궤도를 거친 후 지구-달 천이 궤적으로 진입하는 방법을 모두 이용하였다. 아울러 TLI(Trans Lunar Injection) 기동시 탐사선의 대전 지상국에서의 가시성에 따른 기동의 크기에 대한 영향이 분석되었다. 이 연구를 통한 임무 설계 결과는 달 탐사 임무 설계를 위한 발사 가능 시기(launch opportunity), 성공적인 임무 수행을 위한 임무 단계별 최적의 기동량 및 해당 궤도의 특성 그리고 다양한 임무 파라미터등의 해석을 포함하고 있다. 임무 설계 결과, 미래 한국이 쏘아 올릴 수 있는 달 탐사선의 전체 질량은 해당 임무의 수행시기 보다는 초기 지구 출발 궤도의 초기 고도와 발사제의 초기 궤도 투입 성능에 따라 더욱 크게 좌우됨을 확인하였다.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 1994년도 Proceedings of the Korea Automatic Control Conference, 9th (KACC) ; Taejeon, Korea; 17-20 Oct. 1994
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• pp.89-94
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• 1994

This paper presents an impact control algorithm for reducing the potentially damaging effects by interation of redundant manipulators with their environments. In the. proposed control algorithm, the redundancy is resolved at the torque level by locally minimizing joint torque, subject to tire operational space dynamic formulation which maps tire joint torque set into the operational forces. For a given pre-impact velocity of the manipulator, the proposed approach is on generating joint space trajectories throughout the motion near the contact which instantaneously minimize the impulsive force which is a scalar function of manipulator's configurations. This is done by using the null space dynamics which does not affect the motion of an end-effector. The comparative evaluation of the proposed algorithm with a local torque optimization algorithm without reducing impact is performed by computer simulation. The simulation results illustrate the effectiveness of the algorithm in reducing both the effects of impact and large torque requirements.

• Journal of Astronomy and Space Sciences
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• 제28권3호
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• pp.203-216
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• 2011

To prepare for a future Korean lunar orbiter mission, semi-optimal lunar capture orbits using finite thrust are designed and analyzed. Finite burn delta-V losses during lunar capture sequence are also analyzed by comparing those with values derived with impulsive thrusts in previous research. To design a hypothetical lunar capture sequence, two different intermediate capture orbits having orbital periods of about 12 hours and 3.5 hours are assumed, and final mission operation orbit around the Moon is assumed to be 100 km altitude with 90 degree of inclination. For the performance of the on-board thruster, three different performances (150 N with $I_{sp}$ of 200 seconds, 300 N with $I_{sp}$ of 250 seconds, 450 N with $I_{sp}$ of 300 seconds) are assumed, to provide a broad range of estimates of delta-V losses. As expected, it is found that the finite burn-arc sweeps almost symmetric orbital portions with respect to the perilune vector to minimize the delta-Vs required to achieve the final orbit. In addition, a difference of up to about 2% delta-V can occur during the lunar capture sequences with the use of assumed engine configurations, compared to scenarios with impulsive thrust. However, these delta-V losses will differ for every assumed lunar explorer's on-board thrust capability. Therefore, at the early stage of mission planning, careful consideration must be made while estimating mission budgets, particularly if the preliminary mission studies were assumed using impulsive thrust. The results provided in this paper are expected to lead to further progress in the design field of Korea's lunar orbiter mission, particularly the lunar capture sequences using finite thrust.

• Biomolecules & Therapeutics
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• 제20권1호
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• pp.125-131
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• 2012

Impulsiveness is an important component of many psychiatric disorders including Attention-deficit/hyperactivity disorder (ADHD). Although the neurobiological basis of ADHD is unresolved, behavioral tests in animal models have become indispensable tools for improving our understanding of this disorder. In the punishment/extinction paradigm, impulsivity is shown by subjects that persevere with responding despite punishment or unrewarded responses. Exploiting this principle, we developed a new behavioral test that would evaluate impulsivity in the most validated animal model of ADHD of the Spontaneously Hypertensive rat (SHR) as compared with the normotensive "control" strain, the Wistar Kyoto rat (WKY). In this paradigm we call the Electro-Foot Shock aversive water Drinking test (EFSDT), water-deprived rats should pass over an electrified quadrant of the EFSDT apparatus to drink water. We reasoned that impulsive animals show increased frequency to drink water even with the presentation of an aversive consequence (electro-shock). Through this assay, we showed that the SHR was more impulsive than the WKY as it demonstrated more "drinking attempts" and drinking frequency. Methylphenidate, the most widely used ADHD medication, significantly reduced drinking frequency of both SHR and WKY in the EFSDT. Thus, the present assay may be considered as another behavioral tool to measure impulsivity in animal disease models, especially in the context of ADHD.