• 제목/요약/키워드: azimuth

검색결과 794건 처리시간 0.021초

GPS측량에 의한 경위도원점의 신원방위각 결정 및 정확도 분석 (Determination of New Azimuth on the Suwon Geodetic Datum by GPS Surveying and Its Accuracy Analysis)

  • 최윤수;박병욱;김경수;강인구;안영길;조현천
    • 한국측량학회지
    • /
    • 제17권4호
    • /
    • pp.403-410
    • /
    • 1999
  • 우리나라의 원방위점이 주변지역의 개발로 인하여 시통이 불가능하게 되어 새로운 원방위점의 설정과 원방위각의 결정이 불가피한 실정이다. 따라서 본 연구에서는 측점간의 시통문제와 기상문제에서 탈피하여 정확도, 경제성 등에서 효율적인 GPS를 이용하여 수원원점의 신원방위각을 결정하였다. 즉, 외국 문헌조사를 토대로 GPS를 이용한 방위각결정에 관한 작업규정을 우리나라 실정에 맞도록 수정ㆍ보완하였으며 이에 따라 GPS 관측망을 구성ㆍ관측하여 신원방위각을 결정하고 정확도를 분석하였다.

  • PDF

전달정렬 함상 발사 고속 유도무기의 보정필터 설계에 대한 연구 (A Study on the Design of Correction Filter for High-Speed Guided Missile Firing from Warship after Transfer Alignment)

  • 김천중;이인섭;오주현;유해성;박흥원
    • 전기학회논문지
    • /
    • 제68권1호
    • /
    • pp.108-121
    • /
    • 2019
  • This paper presents the study results on the design of the correction filter to improve the azimuth error estimation of the high-speed guided missile launched from the warship after the transfer alignment. We theoretically proved that the transfer alignment performance is determined by the accuracy of the marine inertial navigation system and the observability of the attitude error state variable in the transfer alignment filter, and that most of navigation errors in high-speed guided missile are caused by azimuth error. In order to improve the azimuth estimation performance of the correction filter, the multiple adaptive estimation method and the adaptive filters adapting the measurement noise covariance or the process noise covariance are proposed. The azimuth estimation performance of the proposed adaptive filter and the existing Kalman filter are compared and analyzed each other for 8 different transfer alignment accuracy cases. As a result of comparison and analysis, it was confirmed that the adaptive filter adapting the process noise covariance has the best azimuth estimation performance. These results can be applied to the design of correction filters for high-speed guided missile.

Geolocation Error Analysis of KOMPSAT-5 SAR Imagery Using Monte-Carlo Simulation Method

  • Choi, Yoon Jo;Hong, Seung Hwan;Sohn, Hong Gyoo
    • 한국측량학회지
    • /
    • 제37권2호
    • /
    • pp.71-79
    • /
    • 2019
  • Geolocation accuracy is one of the important factors in utilizing all weather available SAR satellite imagery. In this study, an error budget analysis was performed on key variables affecting on geolocation accuracy by generating KOMPSAT-5 simulation data. To perform the analysis, a Range-Doppler model was applied as a geometric model of the SAR imagery. The results show that the geolocation errors in satellite position and velocity are linearly related to the biases in the azimuth and range direction. With 0.03cm/s satellite velocity biases, the simulated errors were up to 0.054 pixels and 0.0047 pixels in the azimuth and range direction, and it implies that the geolocation accuracy is sensitive in the azimuth direction. Moreover, while the clock drift causes a geolocation error in the azimuth direction, a signal delay causes in the range direction. Monte-Carlo simulation analysis was performed to analyze the influence of multiple geometric error sources, and the simulated error was up to 3.02 pixels in the azimuth direction.

Designation of the Boundary Conditions for Estimating the Thrust Loss due to Thruster-Hull Interactions

  • Gi Su Song;Seung Jae Lee;Ju Sung Kim
    • 한국해양공학회지
    • /
    • 제36권6호
    • /
    • pp.353-363
    • /
    • 2022
  • The azimuth thruster is mainly installed on a vessel that requires a dynamic positioning (DP) function for special purposes. When the azimuth thruster on a vessel operates for DP, the thrust loss is induced by the thruster-hull interaction. This study examined the influence of boundary conditions in numerical simulations for predicting thrust loss. Wind turbine installation vessels (WTIV) and floating production storage and offloading (FPSO) were chosen as a target vessels. In this study, two types of boundaries were defined. The first consideration is that the boundary condition was assigned with consideration of the azimuth angle of the thruster, whereas it is fixed regardless azimuth angle of the thruster. The predicted thrust loss according to these boundary conditions showed a difference. This observation originated from the current load of the vessel. Therefore, the boundary conditions for which the current load is not induced need to be designated to obtain a realistic thrust loss in a numerical simulation.

뉴럴-퍼지제어기법에 의한 두 구동휠을 갖는 이동형 로보트의 자세 및 속도 제어 (The Azimuth and Velocity Control of a Mobile Robot with Two Drive Wheels by Neural-Fuzzy Control Method)

  • 조용길;배종일
    • 동력기계공학회지
    • /
    • 제2권3호
    • /
    • pp.74-82
    • /
    • 1998
  • This paper presents a new approach to the design of speed and azimuth control of a mobile robot with two drive wheels. The proposed control scheme uses a Gaussian function as a unit function in the neural-fuzzy network and back propagation algorithm to train the neural-fuzzy network controller in the framework of the specialized learning architecture. It is proposed to a learned controller with two neural-fuzzy networks based on an independent reasoning and a connection net with fixed weights to simplify the neural-fuzzy network. The performance of the proposed controller can be seen by the computer simulation for trajectory tracking of the speed and azimuth of a mobile robot driven by two independent wheels.

  • PDF

Moonpool과 Azimuth Thruster를 장치한 Drillship의 저항추진성능 (Performance of Drillship with Moonpool and Azimuth Thrusters)

  • 유재훈;최순호
    • 대한조선학회논문집
    • /
    • 제41권6호
    • /
    • pp.33-39
    • /
    • 2004
  • The performance of a deep water drillship, is investigated with the view of the characteristics of the thrusters and the resistance increasement due to moonpooi. The model tests have been performed to obtain the resistance of two drillships with the moonpooi open and closed including shape changes of moonpool step. To design the DP system, thrust forces of azimuth thrusters have been measured during azimuthing at zero speed condition. Thrusters, azimuthing under the bottom of ship, have the interactions of the other thrusters due to flow changes made by other thrusters, and the existence of ship hull makes the thrust deduction higher than when the thrust operates by itself. The resistance increasement due to the moonpooi is highly dependent on the step height of the moonpool and the draft. It is found that the height of moonpool step can reduce the resistance increasement by moonpool.

Direction of Arrival Estimation of GNSS Signal using Dual Antenna

  • Ong, Junho;So, Hyoungmin
    • Journal of Positioning, Navigation, and Timing
    • /
    • 제9권3호
    • /
    • pp.215-220
    • /
    • 2020
  • This paper deal with estimating the direction of arrival (DOA) of GNSS signal using two antennae for spoofing detection. A technique for estimating the azimuth angle of a received signal by applying the interferometer method to the GPS carrier signal is proposed. The experiment assumes two antennas placed on the earth's surface and estimates the azimuth angle when only GPS signal are received without spoofing signal. The proposed method confirmed the availability through GPS satellite placement simulation and experiments using a dual antenna GPS receiver. In this case of using dual antenna, an azimuth angle ambiguity of the received signal occurs with respect to the baseline between two antennas. For this reason, the accurate azimuth angle estimation is limits, but it can be used for deception by cross-validating the ambiguity.

뉴럴-퍼지제어기법에 의한 두 구동휠을 갖는 이동 로봇의 자세 및 속도 제어 (The Azimuth and Velocity Control of a Movile Robot with Two Drive Wheel by Neutral-Fuzzy Control Method)

  • 한성현
    • 한국해양공학회지
    • /
    • 제11권1호
    • /
    • pp.84-95
    • /
    • 1997
  • This paper presents a new approach to the design speed and azimuth control of a mobile robot with drive wheel. The proposed control scheme uses a Gaussian function as a unit function in the fuzzy-neural network, and back propagation algorithm to train the fuzzy-neural network controller in the frmework of the specialized learning architecture. It is proposed a learning controller consisting of two neural network-fuzzy based on independent reasoning and a connection net with fixed weights to simple the neural networks-fuzzy. The performance of the proposed controller is shown by performing the computer simulation for trajectory tracking of the speed and azimuth of a mobile robot driven by two independent wheels.

  • PDF

아지무스 추진기의 감속 기어 윤활용 오리피스 파이프 진동특성과 방진대책 (Vibration Characteristics and its Countermeasure of Orifice Pipe for Reduction Gear Lubrication of Azimuth Thruster)

  • 엄기탁;로날드 디 바로;이돈출
    • 한국소음진동공학회:학술대회논문집
    • /
    • 한국소음진동공학회 2013년도 춘계학술대회 논문집
    • /
    • pp.555-558
    • /
    • 2013
  • A type of electric propulsion employed by specialized purpose vessels or offshore is the azimuth thruster. Azimuth thruster application had been increasing recently and resulted to excellent vessel maneuverability. However, this system is very complex and some of its major component being exposed under the seawater level presents difficulty in sealing design. For Polar class icebreaker operating in extreme sea condition, this requires a high level of reliability and safety. In this study, the characteristics of lubricating orifice pipe structural vibration installed at the lower reduction gear were investigated and analyzed through beam analysis theory and comparison of experiments. Propeller excitation and the resonant modes of vibration causing excessive vibration and suitable countermeasures to prevent damage due to vibration fatigue on the pipe are presented.

  • PDF

광영역 탐지용 35GHz 마이크로스토립 3-dB 테이퍼 배열 안테나 (Microstrip 3-dB Tapered Array Antenna with Wide Detection Range at 35 GHz)

  • 이영주;정명숙;박위상;최재현
    • 한국전자파학회논문지
    • /
    • 제11권6호
    • /
    • pp.984-989
    • /
    • 2000
  • 본 논문은 35GHz에서 동작하는 이동 목표물 추적용 마이크로스트립 배열 안테나에 대해 기술하였다. 넓은 범위에서 목표물을 탐지하기 위해 안테나는 azimuth 방향으로는 넒은 빔 폭이 넓은 E-plane 방향으로 배열하였으며, 3-dB 테이퍼 급전구조를 이용하여 비교적 간단하게 배열 안테나의 side-lobe level (SLL)를 -20dB이하로 하였으며, 동시에 azimuth 방향으로 12.8$^{\circ}$로 넓은 빔 폭을 얻도록 하였다.

  • PDF