• 제목/요약/키워드: payload variation

검색결과 40건 처리시간 0.021초

Chattering에 의한 위성 탑재체 지향성능저하 최소화를 위한 반능동제어기법 성능분석 (Performance Investigation of Semi-Active Control Logic to Minimize a Pointing Performance Degradation of On-Board Payload by Chattering Effects)

  • 오현웅;최영준
    • 한국항공우주학회지
    • /
    • 제38권9호
    • /
    • pp.882-889
    • /
    • 2010
  • 수동형 진동제어 방식과 같이 시스템이 안정되며, 수동형에 비해 높은 제진 효과가 기대되는 반능동 진동제어 방식은 시스템의 안정화가 요구되는 우주구조물의 제진방법에 유효한 진동제어 방식중 하나이다. On-Off 제어방식에 근거한 반능동 제어는 On-Off 스위칭 시에 전달력의 불연속성으로 인한 chattering을 발생시킬 수 있으며, 이는 탑재체 구조물의 고유진동수와의 커플링으로 인하여 지향성능을 저하시키는 원인으로 작용할 수 있다. 본 논문에서는 chattering 영향 최소화를 통한 지향성능향상을 목적으로 LQ(Linear Quadratic)이론에 기반한 가변 감쇠형 반능동 제어기법을 제안하였다. 시뮬레이션 결과는 본 논문에서 제안한 반능동 제어기법은 기존의 skyhook와 LQ를 기반으로 하는 Bang-Bang 반능동 제어기법과 비교하여 높은 진동절연 성능을 나타내고 있다.

CPTR용 카세그레인 오프셋 복 반사경의 해석 (Analysis of Cassegrain Dual Offset Reflectors for Compact Payload Test Range)

  • 노성민;최학근;임성빈
    • 한국전자파학회논문지
    • /
    • 제19권1호
    • /
    • pp.46-53
    • /
    • 2008
  • 일반적으로 카세그레 인 오프셋 복 반사경(Cassegrain Dual Offset Reflector)은 위성 통신용 안테나로 사용되지만, 여기서는 CPTR(Compact Payload Test Range)을 위한 반사경 시스템으로 해석하였다. 시험 영역의 근접 전계는 물리 광학법(Physical Optics)을 적용하여 계산하였다. CPTR은 균일한 평면파 제공을 목적으로 하며, 이를 위해 최소한의 진폭과 위상 리플(ripple)을 가져야 하며, 교차 편파 또한 작아야 한다. 따라서 본 논문에서는 반사경 구조 및 시험 영역의 위치에 따른 근접 전계 패턴을 구하여 전계의 리플, 테이퍼와 교차 편파를 고찰하였다. 특히 통신용 반사경 안테나에서는 나타나지 않는 안테나 축방향의 교차 편파 성분을 고찰하였다.

A Study on Real Time Working Path Control of Vertical Type Robot System for the Forging and Casting Process Automation

  • Lim, O-Deuk;Kim, Min-Seong;Jung, Yang-Geun;Kang, Jung-Suk;Won, Jong-Bum;Han, Sung-Hyun
    • 한국산업융합학회 논문집
    • /
    • 제20권3호
    • /
    • pp.245-256
    • /
    • 2017
  • In this study, we describe a new approach to real-time implementation of working path control for the forging and casting manufacturing process by vertical type articulated robot system. The proposed control scheme is simple in structure, fast in computation, and useful for real-time control of factory automation based on robot system. Moreover, this scheme does not require any accurate parameter information, nor values of the uncertain parameters and payload variations. Reliability of the proposed controller is proved by simulation and experimental results for robot manipulator consisting of arm with six degrees of freedom under the variation of payloads and tracking trajectories in Cartesian space and joint space. The vertical type articulated robot manipulator with six axes made in SMEC Co., Ltd. has been used for real-time implementation test to illustrate the enhanced working path control performance for unmanned automation of the forging and casting manufacturing process.

산업용 로보트매니플레이터 제어기의 성능향상에 관한 연구 (A Stduy on the Performance Inprovement of Industrial Robot Manipulator Controller)

  • 한성현;이만형
    • 한국정밀공학회지
    • /
    • 제7권4호
    • /
    • pp.85-102
    • /
    • 1990
  • Up to now, most robot control systems are very naive. They consist of a number of independent position-servo loops to control each joint angle separately. Those control systems have constant predefined gains and do not cover the complex dynamic interactions between manipulator joints. As a result, the manipulator is severely limited in range of application, speed of operation and variation of payload. This study proposed a new method to design a robot manipulator controller capable of tracking the reference trajectories of joint angles in a reasonable accuracy to cope with actual situations of varying payload, uncertain parameters. The adaptive model following control method has been used to improve existing robot manipulator controllers. The proposed controller is operated by adjusting its gains based on the response of the manipulator in such a way that the manipulator closely matches the reference model trajectories defined by the designer. The stability of adaptive controller is based on the Second Method of Lyapunov. The coupling among joints and the nonlinearity in the dynamic equation are explicitly considered. The designed manipulator controller shows good tracking performance under various load varia- tion and parameter uncertainties.

  • PDF

Vignetting Analysis of GOCI Optical System

  • Yeon, Jeoung-Heum;Youn, Heong-Sik
    • 대한원격탐사학회:학술대회논문집
    • /
    • 대한원격탐사학회 2007년도 Proceedings of ISRS 2007
    • /
    • pp.195-198
    • /
    • 2007
  • GOCI(Geostationary Ocean Color Imager) is the core paryload of the geostationary satellite COMS(Communication, Ocean and Meteological Satellite) for ocean monitoring. It is scheduled to be launched at the end of 2008. GOCI observes ocean color around the Korean Peninsula over $2500km{\times}2500km$ area. Whole field of view is divided into 16 solts and scan mechanism enables to point each slot position. Tilted two-axis scan method is used to observe entire field of view with great pointing stability. Vignetting of the optical system appears when the partial obscuration by intermediate optical components occurs. It leads to the variation of the illumination in the image and gradual fading near the edge of the field. It should be prohibited for the stable radiometric performances. In this work, vignetting analysis of GOCI optical system is performed. For the systematic approach, GOCI optical system is divided into scan mechanism part and telescope part. Vignetting analysis of each part is performed and each result is combined for the overall vignetting performances. The analyzed results can be applied to the selection of slot acquisition angle of scan mechanism to minimize vignetting effects.

  • PDF

Ku-대역 위성중계기용 전압제어형 PIN 다이오드 감쇄기 및 온도보상회로 설계 (Voltage-Controlled PH Diode Attenuator and Temperature Compensation Circuit for Ku-band Satellite Payload)

  • 장병준;염인복;이성팔
    • 한국전자파학회논문지
    • /
    • 제13권5호
    • /
    • pp.484-491
    • /
    • 2002
  • 본 연구에서는 Ku-대역 위성통신 중계기에 사용되는 전압제어형 PIN 다이오드 감쇄기를 설계, 제작, 측정하고 이 감쇄기의 온도 특성 변화를 보상하기 위한 온도보상회로를 제안하였다. PIN 다이오드 감쇄기는 박막 하이브리드 기술을 이용하여 설계되었으며 PIN 다이오드 감쇄기를 전압제어형으로 사용할 경우 최대 선형 특성을 얻을 수 있는 부하 저항(R$_{L}$)의 값을 Simulation 및 실험에 의해 결정되었다. 최적의 부하 저항값은 사용한 PIN 다이오드의 특성에 의해 달라지며, 본 논문에서 사용한 APD-0805의 경우 150$\Omega$의 부하저항으로 PIN 다이오드 한 개에 10 dB 까지 선형 감쇄범위를 얻을 수 있었다. 또한 부하 저항을 포함한 PM 다이오드 감쇄기의 온도 특성을 측정하였고, 측정결과 관찰된 PIN 다이오드 감쇄기가 전압제어형으로 사용되어질 경우의 가장 큰 단점인 온도 특성의 심각한 변화를 보상할 수 있는 온도보상회로를 제안하였다. 제안된 온도보상회로를 갖는 PIN 다이오드 감쇄기는 동작온도에 대해 선형적인 특성을 보이며 동작온도 범위에 걸쳐 0.6 dB 이하의 오차만을 가짐을 확인하였다.

높은 입사 음압 및 설계 인자의 변화에 따른 미세 천공판 흡음 기구의 흡음 특성 (Absorption Characteristics of Micro-perforated Panel Absorber According to High Incident Pressure Magnitude and Variation of Geometric Parameters)

  • 박순홍;서상현
    • 한국소음진동공학회논문집
    • /
    • 제21권11호
    • /
    • pp.1059-1066
    • /
    • 2011
  • The micro-perforated panel absorber(MPPA) is one of promising noise control elements because of its applicability to extreme environments where general porous materials cannot be used. Since the MPPA is inherently non-porous sound absorber, it can be a good candidate of acoustic protection system of a space launcher. The overall sound pressure level inside payload fairings of commercial launch vehicles is so high(around 140 dB OASPL) that the conventional linear impedance model cannot be directly applied to the design of the acoustic protection systems. In this paper an acoustic impedance models of a micro-perforated panel absorber at high sound pressure environment were reviewed and the use of the impedance on the practical design of MPPAs was addressed. The variation of absorption characteristics of MPPA was discussed according to the design parameters, e.g., perforation ratio, the minute hole diameter, the thickness of MPP and the incident sound pressure level.

Storm-Time Behaviour of Meso-Scale Field-Aligned Currents: Case Study with Three Geomagnetic Storm Events

  • Awuor, Adero Ochieng;Baki, Paul;Olwendo, Joseph;Kotze, Pieter
    • Journal of Astronomy and Space Sciences
    • /
    • 제36권3호
    • /
    • pp.133-147
    • /
    • 2019
  • Challenging Minisatellite Payload (CHAMP) satellite magnetic data are used to investigate the latitudinal variation of the storm-time meso-scale field-aligned currents by defining a new metric called the FAC range. Three major geomagnetic storm events are considered. Alongside SymH, the possible contributions from solar wind dynamic pressure and interplanetary magnetic field (IMF) $B_Z$ are also investigated. The results show that the new metric predicts the latitudinal variation of FACs better than previous studies. As expected, the equatorward expansion and poleward retreat are observed during the storm main phase and recovery phase respectively. The equatorward shift is prominent on the northern duskside, at ${\sim}58^{\circ}$ coinciding with the minimum SymH and dayside at ${\sim}59^{\circ}$ compared to dawnside and nightside respectively. The latitudinal shift of FAC range is better correlated to IMF $B_Z$ in northern hemisphere dusk-dawn magnetic local time (MLT) sectors than in southern hemisphere. The FAC range latitudinal shifts responds better to dynamic pressure in the duskside northern hemisphere and dawnside southern hemisphere than in southern hemisphere dusk sector and northern hemisphere dawn sector respectively. FAC range exhibits a good correlation with dynamic pressure in the dayside (nightside) southern (northern) hemispheres depicting possible electrodynamic similarity at day-night MLT sectors in the opposite hemispheres.

Variation of the Hemispheric Asymmetry of the Equatorial Ionization Anomaly with Solar Cycle

  • Kwak, Young-Sil;Kil, Hyosub;Lee, Woo Kyoung;Yang, Tae-Yong
    • Journal of Astronomy and Space Sciences
    • /
    • 제36권3호
    • /
    • pp.159-168
    • /
    • 2019
  • In solstices during the solar minimum, the hemispheric difference of the equatorial ionization anomaly (EIA) intensity (hereafter hemispheric asymmetry) is understood as being opposite in the morning and afternoon. This phenomenon is explained by the temporal variation of the combined effects of the fountain process and interhemispheric wind. However, the mechanism applied to the observations during the solar minimum has not yet been validated with observations made during other periods of the solar cycle. We investigate the variability of the hemispheric asymmetry with local time (LT), altitude, season, and solar cycle using the electron density taken by the CHAllenging Minisatellite Payload satellite and the global total electron content (TEC) maps acquired during 2001-2008. The electron density profiles provided by the Constellation Observing System for Meteorology, Ionosphere, and Climate satellites during 2007-2008 are also used to investigate the variation of the hemispheric asymmetry with altitude during the solar minimum. During the solar minimum, the location of a stronger EIA moves from the winter hemisphere to the summer hemisphere around 1200-1400 LT. The reversal of the hemispheric asymmetry is more clearly visible in the F-peak density than in TEC or in topside plasma density. During the solar maximum, the EIA in the winter hemisphere is stronger than that in the summer hemisphere in both the morning and afternoon. When the location of a stronger EIA in the afternoon is viewed as a function of the year, the transition from the winter hemisphere to the summer hemisphere occurs near 2004 (yearly average F10.7 index = 106). We discuss the mechanisms that cause the variation of the hemispheric asymmetry with LT and solar cycle.

Flight Model Development of the MIRIS, the Main Payload of STSAT-3

  • 한원용;이대희;박영식;정웅섭;문봉곤;박귀종;박성준;표정현;이덕행;남욱원;박장현;선광일;양순철;박종오;이승우;이명목
    • 천문학회보
    • /
    • 제37권1호
    • /
    • pp.65.1-65.1
    • /
    • 2012
  • MIRIS (Multipurpose Infra-Red Imaging System) is the first Korean Infrared Space Telescope developed by KASI (Korea Astronomy and Space Science Institute), and is the main payload of STSAT-3 (Science and Technology Satellite-3). The FM (fight model) of MIRIS has been recently completed, and various performance tests have been made to measure system parameters such as readout noise, system gain, linearity, and dark current. Final thermal-vacumm test of the MIRIS and the vibration test of the electronics box have been performed. Band response tests showed good agreement with the initial design requirements. No significant dark difference was measured within the expected temperature variation range during observation in orbit. Using Pa-alpha band from a uniform source, the readout noise and system gain were measured by mean variance test. To obtain uniform flat image, flat fielding tests were made for each band, and the data will be compared to that obtained in orbit for calibration. The final version of MIRIS FM will be delivered in March, and it will be integrated into the satellite system for the AIT (Assembly Integration, Test) procedure. The launch of MIRIS is expected in November 2012.

  • PDF