• 한국군사과학기술학회지
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• 제16권2호
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• pp.101-110
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• 2013

This paper considers the many kinds of attitude control systems including launcher. JVC(Jet vane control), Jet tap, Jetvator and Movable nozzles are used to control the initial attitude of a missile only. Recently side jet thruster and it's applications to control initial turn and to maneuver at high altitude have been increased. How to design and develop the missile for an initial turn and a high maneuver at high altitude using side jet thrust were described in this paper.

• 한국항공우주학회지
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• 제41권2호
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• pp.107-119
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• 2013

네 개의 반작용휠과 두 개의 제어모멘트자이로를 이용하여 2축 고기동을 포함한 3축 자세제어방법을 연구하였다. 두 개의 제어모멘트자이로 때문에 발생하는 특이점에 대해 살펴보고 특이점을 탈출하는 방법을 제안하였다. 이 결과를 토대로 고기동을 위한 구동기 제어방법을 제안하였다. 아울러 자세제어 전후의 반작용휠과 제어모멘트자이로의 모멘텀이 유지되도록 하는 구동기 모멘텀 관리방법도 제안하였다. 시뮬레이션을 통하여 설계된 제어기법이 위성의 3축 제어 및 2축에 대한 고기동을 달성하며 구동기의 모멘텀도 보전하는 것을 확인하였다.

• The Journal of Korean Physical Therapy
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• 제34권5호
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• pp.205-211
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• 2022

Purpose: This study investigated the effects of an intervention that combined the abdominal drawing-in maneuver and frequency-specific neuromuscular electrical stimulation on changes in trunk muscle activity, muscle fatigue, and balance in stroke patients. Methods: Thirty stroke patients were randomly assigned to two groups. Fifteen subjects were assigned to group I which performed the abdominal drawing-in maneuver combined with low-frequency neuromuscular electrical stimulation and the other 15 subjects to group II where the abdominal drawing-in maneuver was combined with high-frequency neuromuscular electrical stimulation. Muscle activity and fatigue were measured using surface electromyography before the intervention. Balance was measured using the Trunk Impairment Scale and re-measured after six weeks of intervention for comparative analysis. Results: Both groups showed a significant increase in muscle activity and balance (p<0.05), and there was no significant difference between the groups (p>0.05). In the changes in muscle fatigue, only the experimental group II showed a significant increase in muscle fatigue (p<0.05). The difference between the groups was statistically significant (p<0.05). Conclusion: It was confirmed that among stroke patients, the combination of the abdominal drawing-in maneuver and low-frequency neuromuscular electrical stimulation was more effective in changing the muscle activity and balance of the trunk by minimizing the occurrence of muscle fatigue compared to the combination of the abdominal drawing-in maneuver and high-frequency stimulation. These results can be used as basic data for clinical trunk stabilization training.

• 제어로봇시스템학회논문지
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• 제5권3호
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• pp.370-378
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• 1999

KOMPSAT is a three-axis stabilized light weight satellite, and one of the main mission objectives of the KOMPSAT is to conduct scientific and technological analysis in the areas of high resolution imaging and ocean color imaging. This kind of mission requires the satellite to roll up to 45 degrees. Bang-bang control for this rolling maneuver may activate the flexible modes, and therefore cause satellite pointing performance degradation. To deal with this problem, the roll attitude control system, especially for the science mode and maneuver mode of the KOMPSAT, is first verified by numerical simulation. And the open-loop control law for roll maneuver is proposed by use of series expansion and optimization. The proposed control law is applied to KOMPSAT to see its effectiveness.

• 대한전기학회:학술대회논문집
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• 대한전기학회 2002년도 하계학술대회 논문집 D
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• pp.2096-2098
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• 2002

In this paper, the optimal evasive maneuver strategies for typical subsonic ASM(anti-ship missile) to reach its target ship with high survivability against CIWS(close in weapon system) are studied. The optimal evasive maneuver input is defined by the homing command optimizing the cost function which takes aiming errors of CIWS into account. The optimization problem for the effective evasive maneuver is formulated based on a simple missile dynamics model and a CIWS model. By means of solving the problem, a multiple hypotheses testing method is proposed. Since this method requires generation of too many hypotheses, the hypothesis-pruning technique is adopted. The solution shows that the optimal evasive maneuver is a bang-bane shaped command whose frequency is varied by the aimpoint determination strategy in CIWS.

• Korean Journal of Otorhinolaryngology-Head and Neck Surgery
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• 제61권12호
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• pp.658-662
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• 2018

Background and Objectives The early assessment of treatment is not done for benign paroxysmal positional vertigo (BPPV) since the well-known phenomenon of fatigability after a repeated positional test can mimic successful treatment. The aim of this study is to evaluate the clinical implication of 'fatigability' after Epley maneuver and to identify the therapeutic efficacy of Epley maneuver in posterior canal BPPV (PC-BPPV). Subjects and Method This study was prospectively conducted by two dizziness clinics on 51 consecutive patients diagnosed with PC-BPPV. All patients included in the study received Epley maneuver treatment. The therapeutic results were reassessed immediately after a single trial of Epley maneuver. After 30 minutes, results were reassessed repeatedly to confirm the fatigability of diagnostic procedure immediately after treatment. If the treatment was not successful after 30 minutes, Epley maneuver was repeatedly performed until complete resolution. Results Immediately after the first maneuver, 45 of 51 (88.2%) patients had neither vertigo nor nystagmus during the positional test. All patients demonstrated complete resolution after receiving one to three Epley maneuvers on the day of diagnosis. 'Fatigability (false negative result)' was confirmed for only one case (1 of 6 patients, 16.7%), in which nystagmus was observed after 30 minutes but not identified immediately after the first Epley maneuver. Conclusion The therapeutic efficacy of Epley maneuver is very high in PC-BPPV. Considering the possibility of fatigability when reassessment is performed immediately after therapeutic maneuver, clinicians should avoid assessing the outcome immediately after treatment in patients with PC-BPPV.

• 한국항공우주학회지
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• 제43권7호
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• pp.648-656
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• 2015

능동 합성개구레이더 위성의 주요기동은 SAR 안테나 방향을 바꾸기 위한 롤축 기동이다. 그리고 도플러 중심주파수 변화를 최소화하기 위하여 요축 기동이 요구된다. 따라서 토크/모멘텀 용량을 대부분 롤축으로 그 다음으로 요축으로 할당하는 것이 합리적이다. 하지만 궤도 조정 때문에 가끔씩 피치축으로 중심으로 큰 각도의 회전이 요구된다. 본 논문에서는 롤축과 요축의 연속회전을 통한 피치축 기동시간 단축 방법에 대해서 살펴본다. 이들 두 축이 피치축에 비해서 기동성능이 좋기 때문에, 피치축을 중심으로 큰 회전이 요구될 때는 기동시간 단축이 가능하다.

• 대한조선학회논문집
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• 제42권6호
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• pp.601-607
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• 2005

This paper describes a hydrodynamic modelling study based on the Feldman's equation to predict the nonlinear and coupled maneuvering characteristics of high speed submarine. The hydrodynamic coefficients set is obtained from the modeling of the cross flow drag force and sail induced vorticity, and the captive model experiments(VPMM and RA test) results used to improved the accuracy. The results contained in this paper will be helpful to predict the behavior of tight turn maneuver and to improve the SOE(Safety Operational Envelope) analysis in case of emergency maneuver.

• 한국통신학회논문지
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• 제35권11B호
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• pp.1659-1666
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• 2010

고기동 유도탄들은 다양한 탄내 인터페이스와 빠른 유도 조종 루프를 가진다. 그러므로 Hardware-in-the-Loop(HWIL) 시뮬레이션 제어 시스템은 고성능의 연산기능 및 하드웨어 인터페이스 기능을 가져야 하며, 실시간 운영체제, 임베디드 시스템, 자료 통신, 실시간 하드웨어 제어와 같이 다양한 IT 분야를 융합하여 개발되어야 한다. 이 논문은 고기동 유도탄의 HWIL 시뮬레이션을 수행하기 위한 제어 시스템 설계 기법으로 시스템 하드웨어 구성, 고성능의 다중 프로세서를 사용하기 위한 업무 할당 알고리즘, HWIL 시뮬레이션 실시간 연산 및 제어 기법, 프로세서 통신 기법, 실시간 자료 획득 기법을 제시한다.

• 한국항공우주학회지
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• 제44권9호
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• pp.806-813
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• 2016

위성의 자세제어 및 기동을 위해서는 네 개의 반작용휠을 피라미드 형태로 배치하여 사용하는 것이 일반적이다. 하지만 위성의 관성모멘트가 크거나 사용할 수 있는 반작용휠의 용량이 작은 경우에는 다섯 개의 반작용휠을 사용하는 것을 생각해볼 수 있다. 이 경우, 반작용휠 배치부터 운용방법까지 여러 가지 문제를 다시 고려해야 한다. 능동합성개구레이더 위성은 관측 각도 변화를 위해서 롤축 방향으로 빠른 기동이 요구된다. 본 논문에서는 합성개구레이더 위성의 롤축 방향 기동성능 향상을 위하여 다섯 개의 반작용휠을 배치하는 경우, 이를 운용하는 방법을 연구해본다.