• Journal of Aerospace System Engineering
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• v.16 no.5
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• pp.49-56
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• 2022

S-STEP is a small SAR satellite mission that monitors time-limited emergency targets and military anomalies in areas of interest, achieving the average revisit in less than 30 minutes by deploying a constellation of 32 satellites in low orbit at an altitude of 510 km. The mission operation mode of S-STEP is divided into normal mode, observation mode, communication mode, and orbit maintenance mode. Further,, the attitude control mode is subdivides into initial detumbling, sun pointing, target pointing, ground station pointing, and thrust direction maintenance. Based on the preliminary mission operational scenario and the satellite's characteristics, this study analyzed the attitude control performance during initial detumbling and observation modes. It verifies that each mode's attitude control accuracy requirements within the time allotted by the scenario of the S-STEP achieved.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.38 no.5
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• pp.437-444
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• 2010

This paper deals with the attitude control of an underactuated spacecraft that has one single-gimbal variable-speed CMG. An underactuated spacecraft may not converge to arbitrary attitudes if its total angular momentum is not zero. To stabilize a spacecraft, the CMG has to align with the angular momentum in the inertial frame. Four different install configurations for the CMG have been considered and controllable angular momentums have been analyzed. Also, based on the backstepping method, stabilizing control laws have been presented and their properties have been compared.

• Journal of Veterinary Clinics
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• v.14 no.2
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• pp.238-243
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• 1997

체중이 700-750kg 인 4마리의 중종마에 70분동안 마취를 실시하여 동맥혈의 이 산화탄소 분압과 호기말 가스내의 이산화탄소 분압 사이의 관계를 관찰하였다. 마취도중 자발 호흡, 인공호흡 1(흡기시간 2.0초), 인공호흡 2(흡기시간 2.5초)를 각각 30분,20분,20분씩 실시하였으며 매 10분마다 동맥혈가스분석과 호기말 가스내 이산화탄소분압 측정을 실시하 였다. 동시에 혈압, 심전도, 체온측정을 실시하여 마취된 환축의 상태를 관찰하였다. 2주후에 자세를 달리하여(앙와에서 측와로) 같은 방법으로 재 실험하였다. 호기말 이산화탄소분압은 동맥혈에서보다 평균 10 mmHg 정도 낮은 양상을 보였으나 높은 상관관계를 보였으며 자세에 따른 유의적 차이는 업었다(앙와자세; r=0.949, 측와자세; r=0.920, P<0.01). 이러한 결과를 토 대로 조직에 창상을 줄 수 있는 동맥혈 가스분석 대신 비침습적방법인 호기말 가스내 이산화 탄소 분압을 측정하는 것이 환축의 모니터링에 효과적으로 사용 가능하다는 것을 알 수 있었다.

• The Journal of Korean Society for Radiation Therapy
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• v.23 no.2
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• pp.83-90
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• 2011

Purpose: This study statistically analyzed the difference of the stability of maintaining a respiratory period shown according to position and use of a device to search the tendency and usefulness of a device. Materials and Methods: The study obtained respiratory signals which maintained a respiratory period for 20 minutes each supine and prone position for 11 subjects. The study obtained respiratory signals in a state of using a belly board for 7 patients in a bad condition of a respiratory period in a prone position to analyze a change in respiration and the stability before and after the use of a device. Results: The supine part showed 54.5%, better than the prone part of 36.4% in a case that the stability for maintaining a respiratory period was in a good condition as a fixed respiratory period was well maintained according to the position. 6 patients (85%) showed a maintenance pattern of a respiratory period significantly different before the use and 4 patients showed a significantly good change in the stability for maintaining a respiratory period as a result that belly boards were used for 7 patients that the maintenance of a respiratory period was not in a good condition on a prone position. Conclusion: It seemed that this study could contribute to the maintenance of respiratory period and of respiratory stability as the optimal position for maintenance of respiration and the use of a device such as a belly board were decided through statistic analysis of respiratory signals and its application even if patient position and use of device were decided by the beam arrangement a treatment part of a patient, location of a target, and an expected plan.

• Journal of Astronomy and Space Sciences
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• v.8 no.1
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• pp.85-98
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• 1991

Geomagnetism was used to control the attitude of the small scientific satellite at low altitude in sun-synchronous orbit. First, we analyzed the telemetry data. The rotation state of the satellite, can be known from the magnitude and variations of the magnetic field which is measured from the 3 axis magnetometer. In axisymmetric case, it is possible to control the attitude of the satellite by changing the rotation velocity of each 3 axis. The algorithm and the program were developed to calculate the supply time of the current operating the magnetorquer. This attitude control can be applied when the satellite is in tumbling motion and after passive control is attained by the Gravity gradient boom.

• Bulletin of the Korean Space Science Society
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• 2009.10a
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• pp.29.1-29.1
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• 2009

이 연구는 별 관측을 통해 점 퍼짐 함수(PSF)를 측정하고 나이퀴스트 주파수에서 변조 전달 함수(MTF)을 계산하여 주파수 영역에서 저궤도 광학 위성의 영상품질 평가방법을 도출하였다. 가상 별 영상을 생성하고 IRAF로 2차원의 점 퍼짐 함수를 얻었고 MATLAB으로 점 퍼짐 함수를 2차원 푸리에 변환하여 변조 전달함수를 계산하였다. 공간 영역에서는 점 퍼짐 함수의 모양을 통해서도 영상품질을 검증할 수 있다. Along/Across-Track의 모양이 일치하고 중심에서 좌우대칭이며 델타함수에 가까울수록 좋은 품질의 영상을 의미한다. Along/Across-Track의 점 퍼짐 함수 모양차이는 Line Rate나 Time Delay and Integration(TDI)의 오차에서 기인한다. 별을 점광원으로 본다면 점 퍼짐 함수를 정의하기 쉽고 Along/Across 방향을 동시에 측정 가능하다는 장점이 있다. 궤도상에서 별을 관측하는 것은 지상을 관측하는 것보다 대기 환경의 효과가 크지 않기 때문에 영상 품질 평가에 유리하다. Yaw Steering이나 Nadir Pointing과 같은 자세제어의 효과를 배제할 수 있으므로 자세제어의 효과가 상당 부분 제거된 영상품질을 분석할 수 있다. 지상관측시간이나 배터리 충전시간이 아닌 지구 본영에서 별을 관측하므로 임무에 방해받지 않는다. 지상관측과 같은 효과를 내고 TDI를 사용하는 환경을 구현하기위해 Line Rate를 고려한 자세 기동 방법에 대해 연구하였다. 큰 각도의 자세 기동이 예상되어 쿼터니안을 이용하여 Inertial Pointing하도록 자세 제어하였고, 자세 Slew Rate 구속조건 하에서 제어가 필요하다.

• The Journal of the Convergence on Culture Technology
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• v.5 no.3
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• pp.257-262
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• 2019

Recently, with a great deal of attention and utilization to the UAV like a drone, many application cases using UAV in various fields have been proliferated rapidly. These UAV, however, has many risks like balance deviation and drone crash due to the external environmental factors. The attitude control algorithm for UAV is the most important portion in order to maintain the safe management of UAV, and the best solution is PID control algorithm which is generously used and almost perfect attitude control technology nowadays. In this paper, we propose the smart attitude control algorithm using fuzzy logic in order to provide safe and continuous attitude control against external environmental factors, and compare the performance through simulation study between PID and our algorithm.

• Journal of the Korean Society of Radiology
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• v.7 no.3
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• pp.233-238
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• 2013

Chest lateral decubitus radiation exposure PA be carried out in general, but emergency patient or the patient's discomfort in the body examination had a lot of inconvenience. In this study, we compared AP and PA image quality, patient safety, and analysis of the examination effectiveness between the two tests was to evaluate the usefulness. Pleurisy or pneumothorax in patients with suspected or diagnosed chest lateral decubitus radiation exposure 30 consecutive patients (male 20 patients, 10 females) were included in the study. Image quality evaluation method microstructure of lung, wide areas of diagnosis, a clear air-fluid interface, the patient rotate, cardiac shadow and sharp diaphragmatic was based on Department of Radiology specialist, division of pulmonology resident blind test was evaluated by four people. Chest decubitus by radiation exposure the AP and PA position examination the usefulness of comparative analysis Image quality in the AP and PA, whereas there was no significant difference in attitude, Stability of the patient and Radiation's examination efficiency AP position compared to the position of PA scores were higher. PA position does not require a examination may be of AP position in a position to suggest that.

• Proceedings of the Korean Society for Emotion and Sensibility Conference
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• 2002.11a
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• pp.233-244
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• 2002

The purpose of this study is to assess the ability of balance control in moving surround using head mount device and force platform and to examine the clinical usefulness of COP parameters. Fifteen patients with stroke and healthy persons were participated. COP parameters were obtained as total path distance, frequency of anterior-posterior and medial-lateral component by FFT analysis, weight-spectrum analysis in the two different conditions; (1) in comfortable standing with opened or closed eyes, (2) in virtual moving surround delivered using HMD to four different moving pattern. In virtual moving surround setting, moving pattern was composed of close-far, superior-inferior tilting(pitch), right-left tilting(roll) and horizontal rotation(yaw) movement. In all parameters, the reliebility of COP analysis system was significantly high. Also, the construct validity compared between fifteen patients with stroke and normal persons was excellent in virtual moving surround condition(p

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.37 no.6
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• pp.537-544
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• 2009

This paper concerns analysis technique on determining of attitude control gain in the low frequency region using stability area. The stability area is defined by the D-Decomposition method, which was designed by Neimark. In this paper, it is introduced D-Decomposition method from reference paper and design attitude control gain of generic launch vehicle during first stage flight phase. For selecting PD control gain, it is considered the system parameter uncertainty about whole first-stage flight phase, represented the stability area boundary on each case. After deciding the PD control gain using stability area method, it is applied to launch vehicle linear model, and checking the stability margin requirement, frequency response characteristics.