• 제목/요약/키워드: servo controller

검색결과 924건 처리시간 0.02초

비접촉 동력 전달을 위한 마그네트 기어 기반 감속기의 속도 제어에 관한 연구 (Speed Control Of The Magnet Gear-Based Speed Reducer For Non-contact Power Transmission)

  • 정광석
    • 한국산학기술학회논문지
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    • 제17권7호
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    • pp.380-388
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    • 2016
  • 마그네트 기어를 이용하면 기계적인 접촉없이 동력을 전달할 수 있다. 마그네트 기어 기반 감속 시스템에서 종동축은 구동축으로부터 분리되어있기 때문에 시스템은 제한된 공극 강성으로 부하 변화에 대응해야하는 2관성 공진 시스템이다. 종동축 즉, 저속측은 구동축 인가 토크만으로 제어되고 갑작스런 외란에 따라 일반적인 기계식 기어 시스템과 달리 과도한 진동이나 슬립이 발생할 수 있다. 따라서 저속측에 인가되는 부하 등의 외란은 실시간으로 측정되거나 추정되어야 한다. 본 논문에서는 고조파 조절기 일체형 마그네트 기어를 이용한 감속 시스템의 저속측 속도 제어를 위한 전상태 되먹임 제어기를 제안하고 이를 전산 모의 시험과 실험을 통해 검증하였다. 저속측 부하를 추정하기 위해 새로운 상태변수를 도입하여 관측기를 설계하였으며 이를 기반으로 하는 전상태 제어기를 통한 외란에 대한 강건성은 2자유도 PI 속도 제어기와 비교하였다. 상대적으로 짧은 시간안에 극의 슬립이 보정되는 것을 확인하였으며 추정된 변수는 실제 측정 결과와 유사한 경향을 나타내었다. 이러한 결과는 마그네트 기어 감속기의 서보 시스템으로의 응용 가능성을 담보해주는 결과인 것으로 판단된다.

탄약운반장갑차의 장약 파손 방지를 위한 최적설계에 관한 연구 (A Study on the Optimum Design for Preventing Propelling Charge to Military Ammunition Vehicle)

  • 노상완;김성훈;박영민;김병현
    • 한국산학기술학회논문지
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    • 제20권11호
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    • pp.494-500
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    • 2019
  • 본 연구는 탄약운반장갑차의 장약이송 소프트웨어 최적 설계를 통해 장약이송 시 파손을 방지하는 것을 목표로 하고 있다. 탄약운반장갑차는 자동화된 장약이송시스템이 적용되어 있다. 군 운용 중 장약 적재 시 간헐적으로 장약이 파손되는 현상이 발생하여 다음과 같은 개선방법을 연구하였고, 입증시험을 실시하였다. 장약 이송기의 속도가 높을 경우 충격력이 증가하기 때문에 적재 속도를 기존보다 60% 감소 시켰고, 포스 게이지를 활용하여 충격력을 측정하였다. 충격력 측정 결과 평균 45% 감소하는 것을 확인 할 수 있었다. 적재관 내부의 간섭 등에 의한 이송기의 부하 발생 시 서보제어기의 최대전류 11A를 출력하면 장약이 파손 될 가능성이 있다. 또한, 최대전류가 낮을 경우 장약적재가 불가하기 때문에 적정 값을 찾아야 했고, 이는 시험을 통하여 최적의 최대전류 값 6.5A를 도출하였다. 최적설계 입증 시험에는 종이지관장약과 실제장약을 적용하여 시험 하였다. 종이지관 장약과 실제 장약으로 탄운차에 장약 적재시험을 실시한 결과 장약의 파손이 발생하지 않았으며, 장약 적재가 정상적으로 이루어져 설계 개선이 타당한 것을 입증하였다.

PRELIMINARY FEASIBILITY STUDY OF THE SOLAR OBSERVATION PAYLOADS FOR STSAT-CLASS SATELLITES

  • Moon, Yong-Jae;Cho, Kyung-Seok;Jin, Ho;Chae, Jong-Chul;Lee, Sung-Ho;Seon, Kwang-Il;Kim, Yeon-Han;Park, Young-Deuk
    • Journal of Astronomy and Space Sciences
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    • 제21권4호
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    • pp.329-342
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    • 2004
  • In this paper, we present preliminary feasibility studies on three types of solar observation payloads for future Korean Science and Technology Satellite (STSAT) programs. The three candidates are (1) an UV imaging telescope, (2) an UV spectrograph, and (3) an X-ray spectrometer. In the case of UV imaging telescope, the most important constraint seems to be the control stability of a satellite in order to obtain a reasonably good spatial resolution. Considering that the current pointing stability estimated from the data of the Far ultraviolet Imaging Spectrograph (FIMS) onboard the Korean STSAT-1, is around 1 arc minutes/sec, we think that it is hard to obtain a spatial resolution sufficient for scientific research by such an UV Imaging Telescope. For solar imaging missions, we realize that an image stabilization system, which is composed of a small guide telescope with limb sensor and a servo controller of secondary mirror, is quite essential for a very good pointing stability of about 0.1 arcsec. An UV spectrograph covering the solar full disk seems to be a good choice in that there is no risk due to poor pointing stability as well as that it can provide us with valuable UV spectral irradiance data valuable for studying their effects on the Earth's atmosphere and satellites. The heritage of the FIMS can be a great advantage of developing the UV spectrograph. Its main disadvantage is that two major missions are in operation or scheduled. Our preliminary investigations show that an X-ray spectrometer for the full disk Sun seems to be the best choice among the three candidates. The reasons are : (1) high temporal and spectral X-ray data are very essential for studying the acceleration process of energetic particles associated with solar flares, (2) we have a good heritage of X-ray detectors including a rocket-borne X-ray detector, (3) in the case of developing countries such as India and Czech, solar X-ray spectrometers were selected as their early stage satellite missions due to their poor pointing stabilities, and (4) there is no planned major mission after currently operating Reuven Ramaty High-Energy Solar Spectroscopic Imager (RHESSI) mission. Finally, we present a preliminary design of a solar X-ray spectrometer covering soft X-ray (2 keV) to gamma ray (10 MeV).

측정부위별 신생아의 체온 비교 : 고막기준 직장체온, 직장체온, 액와체온, 복부체온 (Comparison by Measurement Sites in Temperature of Neonates : Ear-based rectal, Rectal, Axilla, Abdominal Temperature)

  • 김화순;안영미
    • 대한간호학회지
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    • 제29권4호
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    • pp.903-916
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    • 1999
  • The purpose of this study was to compare the ear-based rectal temperature measured with a tympanic thermometer with the rectal temperature measured with a glass mercury thermometer in order to test the accuracy of tympanic thermometer and to determine relationship among rectal, axilla, and abdominal temperature in neonates. The samples consisted of thirty four neonates admitted to the neonatal intensive care unit and nursery at an university affiliated hospital. The mean age of the subjects was 4.9 days. The ear-based rectal temperatures were taken with a tympanic thermometer in rectal mode (First Temp Genius 3000). Rectal and axilla temperatures were taken with a glass mercury thermometer, Abdominal temperature was continuously monitored with the probe connected to the servo controller of incubator. The results of the study can be summarized as follows : 1. Intrarater comparison : Agreement between the first and the second ear-based rectal temperature was 97% within 0.1$^{\circ}C$. 2. Comparison of ear-based rectal temperature and the rectal temperature from a glass mercury thermometer : ear-based rectal temperature ranged from 36.95$^{\circ}C$d to 37.95$^{\circ}C$, with a mean of 37.58$^{\circ}C$(SD=0.22$^{\circ}C$). Rectal temperature from a glass mercury thermometer ranged from 36.2$0^{\circ}C$ to 37.2$0^{\circ}C$, with a mean 36.75$^{\circ}C$(SD=0.29). The mean difference between both temperatures was 0.84$^{\circ}C$. The correlation coefficient between both temperatures was r=0.77(p=0.00). 3. Comparison of rectal and axilla temperature : Axilla temperature ranged from 35.8$0^{\circ}C$ to 37.1$0^{\circ}C$, with a mean of 36.55$^{\circ}C$. The mean absolute difference between the rectal and axilla temperature was 0.23$^{\circ}C$. The correlation coefficient between rectal and axilla was r=0.67. 4. Comparison of axilla and abdominal temperature : Abdominal temperature ranged from 36.2$0^{\circ}C$ to 37.0$0^{\circ}C$, with a mean of 36.58$^{\circ}C$. The mean absolute difference between axilla and abdominal temperature was only -0.03$^{\circ}C$. Findings of this study suggest that ear-based rectal temperature overestimates the actual rectal temperatures in neonates. Therefore, the interchangeble use of both temperatures in clinics seems problematic. The site offset(adjustment value) programmed in rectal mode of the tympanic thermometer needs to be readjusted. Choosing one optimal site for temperature measurement for each patient, and using the specific site consistently would result in more consistent measurements of changes in body temperature, and thus can be more effective in diagnosing fever or hypothermia.

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