• 제목/요약/키워드: Angular Filter

검색결과 120건 처리시간 0.026초

확장된 칼만 필터를 이용한 속도 및 검출기가 없는 IPMSM의 최대토크 운전 (Maximum Torque Operation of IPMSM Drives without Speed & Rotor Position Sensors Using An Extended Kalman Filter)

  • 김윤호;윤병도;국윤상
    • 전력전자학회:학술대회논문집
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    • 전력전자학회 1996년도 창립기념 전력전자학술발표회 논문집
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    • pp.21-25
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    • 1996
  • To control the speed of IPMSM drives it is necessary to know the speed and the rotor position. This is normally done by measurement of this values with electromechenical sensors. In this paper, a new approach to the position elimination method for the high performance variable speed IPMSM drives with the current controlled PWM technique is presented. For the high performance drive capability in the speed region, a Extended Kalman filter algorithm is adopted to estimate the rotor position as well as the angular velocity for the practical sensorless IPMSM drives. The high performance drive characteristics of the proposed method are verified using the wide simulation.

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Analysis of the Optimal Frequency Band for a Ballistic Missile Defense Radar System

  • Nguyen, Dang-An;Cho, Byoungho;Seo, Chulhun;Park, Jeongho;Lee, Dong-Hui
    • Journal of electromagnetic engineering and science
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    • 제18권4호
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    • pp.231-241
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    • 2018
  • In this paper, we consider the anti-attack procedure of a ballistic missile defense system (BMDS) at different operating frequencies at its phased-array radar station. The interception performance is measured in terms of lateral divert (LD), which denotes the minimum acceleration amount available in an interceptor to compensate for prediction error for a successful intercept. Dependence of the frequency on estimation accuracy that leads directly to prediction error is taken into account, in terms of angular measurement noises. The estimation extraction is performed by means of an extended Kalman filter (EKF), considering two typical re-entry trajectories of a non-maneuvering ballistic missile (BM). The simulation results show better performance at higher frequency for both tracking and intercepting aspects.

공간지능화에서 다중카메라를 이용한 이동로봇의 인간추적행위 (Human-Tracking Behavior of Mobile Robot Using Multi-Camera System in a Networked ISpace)

  • 진태석;하시모토 히데키
    • 로봇학회논문지
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    • 제2권4호
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    • pp.310-316
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    • 2007
  • The paper proposes a human-following behavior of mobile robot and an intelligent space (ISpace) is used in order to achieve these goals. An ISpace is a 3-D environment in which many sensors and intelligent devices are distributed. Mobile robots exist in this space as physical agents providing humans with services. A mobile robot is controlled to track a walking human using distributed intelligent sensors as stably and precisely as possible. The moving objects is assumed to be a point-object and projected onto an image plane to form a geometrical constraint equation that provides position data of the object based on the kinematics of the intelligent space. Uncertainties in the position estimation caused by the point-object assumption are compensated using the Kalman filter. To generate the shortest time trajectory to track the walking human, the linear and angular velocities are estimated and utilized. The computer simulation and experimental results of estimating and trackinging of the walking human with the mobile robot are presented.

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Geostationary Orbit Surveillance Using the Unscented Kalman Filter and the Analytical Orbit Model

  • Roh, Kyoung-Min;Park, Eun-Seo;Choi, Byung-Kyu
    • Journal of Astronomy and Space Sciences
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    • 제28권3호
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    • pp.193-201
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    • 2011
  • A strategy for geostationary orbit (or geostationary earth orbit [GEO]) surveillance based on optical angular observations is presented in this study. For the dynamic model, precise analytical orbit model developed by Lee et al. (1997) is used to improve computation performance and the unscented Kalman filer (UKF) is applied as a real-time filtering method. The UKF is known to perform well under highly nonlinear conditions such as surveillance in this study. The strategy that combines the analytical orbit propagation model and the UKF is tested for various conditions like different level of initial error and different level of measurement noise. The dependencies on observation interval and number of ground station are also tested. The test results shows that the GEO orbit determination based on the UKF and the analytical orbit model can be applied to GEO orbit tracking and surveillance effectively.

Modified Rodrigues Parameter 기반의 인공위성 관성모멘트 추정 연구 (Spacecraft Moment of Inertial Estimation by Modified Rodrigues Parameters)

  • 방효충
    • 한국항공우주학회지
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    • 제38권3호
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    • pp.243-248
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    • 2010
  • 본 연구에서는 인공위성의 관성 모멘트 추정을 위해 MRP(Modified Rodrigues Parameter) 자세 변수기반의 추정기를 설계하였다. MRP는 인공위성 자세 결정시 쿼터니 언(Quaternion) 파라미터의 구속 조건으로부터 발생하는 필터의 오차 공분산 행렬의 특이(Singularity) 현상을 피할 수 있는 장점이 있다. 한편 MRP의 경우 자세각 변위가 클 경우에 역시 특이현상이 발생할 수 있어 이를 피하기 위해 적절한 자세각 범위에서 인위적인 기준 운동을 생성하여 필터 설계에 적용하였다. 쿼터니언 파라미터의 단점을 극복하여 보다 안정된 오차 공분산 갱신 결과의 필터의 개선된 성능을 예상할 수 있다.

혼합정합 전달정렬시 해상항체의 가관측성 향상조건에 관한 연구 (A study of observability enhancement by matching methods at sea)

  • 김경주;고영웅;박찬웅
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1996년도 한국자동제어학술회의논문집(국내학술편); 포항공과대학교, 포항; 24-26 Oct. 1996
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    • pp.867-870
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    • 1996
  • Often an INS has to be aligned in navigation. In these cases it is necessary to obtain some reference information on the state of the aligned INS(Slave) such as its position, its velocity of its angular rate. Usually the reference information is velocity which is supplied by another reference INS. In the alignment state the velocity computed by the reference INS(Master) is compared with that computed by the slave INS and the difference which is indicative of the slave misalignment with respect to the master, is processed by a Kalman filter which estimates misalignment as well as the slave gyro and accelerometer error states. The operation of aligning a slave INS with a master INS comparing quantities computed by both INS is known as transfer alignment. The delivery vehicle performs error these maneuvers enable the TA Kalman filter to separate between the tilt errors and the accelerometer biases which otherwise are unobservable. The basic objective this paper is to study the observability enhancement by ship's maneuvering and matching methods during transfer alignment at sea.

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A Versatile Universal Capacitor-Grounded Voltage-Mode Filter Using DVCCs

  • Chen, Hua-Pin;Shen, Sung-Shiou
    • ETRI Journal
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    • 제29권4호
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    • pp.470-476
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    • 2007
  • In this paper, a versatile three-input five-output universal capacitor-grounded voltage-mode filter is proposed. The circuit employs two differential voltage current conveyors as active elements together with two grounded capacitors and four resistors as passive elements. The proposed configuration can be used as either a single-input five-output or three-input two-output. Unlike the previously reported works, it can simultaneously realize five different generic filtering signals: lowpass, bandpass, highpass, bandreject, and allpass. It still maintains the following advantages: (i) the employment of all grounded capacitors, (ii) no need to employ inverting-type input signals, (iii) no need to impose component choice, (iv) orthogonal control of the resonance angular frequency ${\omega}_o$ and the quality factor Q, and (v) low active and passive sensitivity performances.

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삼중 사각 루프 슬롯 배열 형태를 갖는 Ka/Ku 대역 주파수 선택 반사기 설계 (Design of Ka/Ku Band Frequency Selective Surface with Triple Square Loop Slot Array)

  • 고지환;조영기
    • 한국전자파학회논문지
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    • 제14권10호
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    • pp.1060-1070
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    • 2003
  • 국내 위성통신용 Ku/Ka 대역 파라볼라 안테나에 적용될 수 있는 삼중 사각 루프 슬롯 배열 형태인 새로운 주파수 선택 반사기 구조를 제시하였다. 본 논문에서 설계, 제작된 주파수 선택 반사기 구조는 다층 유전체인 하니콤 위에 삼중의 사각 루프 슬롯으로 구성되는 단위 소자가 평면에 2차원적으로 주기적인 배열 형태를 지닌다. 주파수 선택 반사기를 제작하여 측정한 결과 계산 결과와 일치되었으며, 요구되는 사양대로 14/12 GHz대 주파수에서는 입사파의 대부분이 투과되는 반면, 30/20 GHz대 주파수에서는 전반사가 일어남을 확인하였다.

A POSITION TRACKING ALGORITHM WITH RADAR MEASUREMENT

  • Lim You-Chol;Ma Keun-Su;Lee Jae-Deuk
    • 한국우주과학회:학술대회논문집(한국우주과학회보)
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    • 한국우주과학회 2004년도 한국우주과학회보 제13권2호
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    • pp.332-336
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    • 2004
  • This paper describes the remote tracking algorithm using measurements (azimuth, elevation, and slant range) of the radar ground station. Kalman filter model for noise reduction of the measured information is first derived by linearizing with respect to angle, angular rate, range, and range rate. And then a tracking algorithm is introduced to calculate the position of the vehicle during in-flight. The simulation results show that the algorithm is practical and effective enough tracking position of the vehicle in considerably less error.

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Highly Angle-tolerant Spectral Filter Based on an Etalon Resonator Incorporating a High Index Cavity

  • Noh, Tae-Hui;Yoon, Yeo-Taek;Lee, Sang-Shin;Choi, Duk-Yong;Lim, Seung-Chan
    • Journal of the Optical Society of Korea
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    • 제16권3호
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    • pp.299-304
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    • 2012
  • A high angular tolerance spectral filter was realized incorporating an etalon, which consists of a $TiO_2$ cavity sandwiched between a pair of Ag/Ge mirrors. The effective angle was substantially extended thanks to the cavity's high refractive index. The device was created by embedding a 313-nm thick $TiO_2$ film in 16-nm thick Ag/Ge films through sputtering, with the Ge layer alleviating the roughness and adhesion of the Ag layer. For normal incidence, the observed center wavelength and transmission were ~900 nm and ~60%, respectively; throughout the range of $50^{\circ}$, the relative wavelength shift and transmission variation amounted to only ~0.06 and ~4%, respectively.