• 제목/요약/키워드: laser navigation

검색결과 182건 처리시간 0.021초

Characteristics of Relative Navigation Algorithms Using Laser Measurements and Laser-GPS Combined Measurements

  • Kang, Dae-Eun;Park, Sang-Young;Son, Jihae
    • Journal of Astronomy and Space Sciences
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    • 제35권4호
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    • pp.287-293
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    • 2018
  • This paper presents a satellite relative navigation strategy for formation flying, which chooses an appropriate navigation algorithm according to the operating environment. Not only global positioning system (GPS) measurements, but laser measurements can also be utilized to determine the relative positions of satellites. Laser data is used solely or together with GPS measurements. Numerical simulations were conducted to compare the relative navigation algorithm using only laser data and laser data combined with GPS data. If an accurate direction of laser pointing is estimated, the relative position of satellites can be determined using only laser measurements. If not, the combined algorithm has better performance, and is irrelevant to the precision of the relative angle data between two satellites in spherical coordinates. Within 10 km relative distance between satellites, relative navigation using double difference GPS data makes more precise relative position estimation results. If the simulation results are applied to the relative navigation strategy, the proper algorithm can be chosen, and the relative position of satellites can be estimated precisely in changing mission environments.

파티클 필터를 이용한 레이저 내비게이션의 위치측정 성능 향상 (Improvement of Positioning Accuracy of Laser Navigation System using Particle Filter)

  • 조현학;김정민;도주철;김성신
    • 한국지능시스템학회논문지
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    • 제21권6호
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    • pp.755-760
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    • 2011
  • 본 논문은 파티클 필터(particle filter)를 이용한 레이저 내비게이션(laser navigation)의 위치측정 성능 향상에 관한 연구이다. 레이저 내비게이션은 무선항법장치(wireless navigation system)로써 무인 자율주행 장치(automatic guided vehicle)의 위치측정 및 제어에 주로 사용되며, 이는 기존의 유선유도장치(wired guidance system)들에 비해 유지보수에 유연하면서도 완전한 자율주행이 가능하다. 하지만 무선항법장치인 레이저 내비게이션은 반응속도가 느리며 고속주행 혹은 회전주행 시에 위치 정밀도가 크게 떨어지게 된다. 본 논문에서는 이와 같은 문제점을 해결하기 위해, 비선형(non-linear)/비가우시안(non-gaussian)의 시스템에서도 강인한 특성을 지닌 파티클 필터를 이용하여 위치 정밀도를 향상시키는 방법을 제안한다. 제안한 방법의 성능을 검증하기 위해, 레이저 내비게이션과 엔코더, 자이로가 장착된 지게차 AGV(automatic guided vehicle)를 사용하였으며, 제안된 방법과 상용화된 레이저 내비게이션의 위치측정 결과를 비교하였다. 실험 결과, 제안된 방법이 상용화된 레이저 내비게이션의 위치 정밀도에 비해 약 66.5% 향상됨을 확인하였다.

Improved GPS-based Satellite Relative Navigation Using Femtosecond Laser Relative Distance Measurements

  • Oh, Hyungjik;Park, Han-Earl;Lee, Kwangwon;Park, Sang-Young;Park, Chandeok
    • Journal of Astronomy and Space Sciences
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    • 제33권1호
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    • pp.45-54
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    • 2016
  • This study developed an approach for improving Carrier-phase Differential Global Positioning System (CDGPS) based realtime satellite relative navigation by applying laser baseline measurement data. The robustness against the space operational environment was considered, and a Synthetic Wavelength Interferometer (SWI) algorithm based on a femtosecond laser measurement model was developed. The phase differences between two laser wavelengths were combined to measure precise distance. Generated laser data were used to improve estimation accuracy for the float ambiguity of CDGPS data. Relative navigation simulations in real-time were performed using the extended Kalman filter algorithm. The GPS and laser-combined relative navigation accuracy was compared with GPS-only relative navigation solutions to determine the impact of laser data on relative navigation. In numerical simulations, the success rate of integer ambiguity resolution increased when laser data was added to GPS data. The relative navigational errors also improved five-fold and two-fold, relative to the GPS-only error, for 250 m and 5 km initial relative distances, respectively. The methodology developed in this study is suitable for application to future satellite formation-flying missions.

Relative Navigation with Intermittent Laser-based Measurement for Spacecraft Formation Flying

  • Lee, Jongwoo;Park, Sang-Young;Kang, Dae-Eun
    • Journal of Astronomy and Space Sciences
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    • 제35권3호
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    • pp.163-173
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    • 2018
  • This paper presents relative navigation using intermittent laser-based measurement data for spacecraft flying formation that consist of two spacecrafts; namely, chief and deputy spacecrafts. The measurement data consists of the relative distance measured by a femtosecond laser, and the relative angles between the two spacecrafts. The filtering algorithms used for the relative navigation are the extended Kalman filter (EKF), unscented Kalman filter (UKF), and least squares recursive filter (LSRF). Numerical simulations reveal that the relative navigation performances of the EKF- and UKF-based relative navigation algorithms decrease in accuracy as the measurement outage period increases. However, the relative navigation performance of the UKF-based algorithm is 95 % more accurate than that of the EKF-based algorithm when the measurement outage period is 80 sec. Although the relative navigation performance of the LSRF-based relative navigation algorithm is 94 % and 370 % less accurate than those of the EKF- and UKF-based navigation algorithms, respectively, when the measurement outage period is 5 sec; the navigation error varies within a range of 4 %, even though the measurement outage period is increased. The results of this study can be applied to the design of a relative navigation strategy using the developed algorithms with laser-based measurements for spacecraft formation flying.

레이저 관성항법장치에서 링레이저 자이로 디더 운동에 의한 가속도계 공진이 자체 정렬/항법 성능에 미치는 영향 분석 (Self-Alignment/Navigation Performance Analysis in the Accelerometer Resonance State Generated by Dither Motion of Ring Laser Gyroscope in Laser Inertial Navigation System)

  • 김천중;임경아;김선아
    • 한국군사과학기술학회지
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    • 제24권6호
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    • pp.577-590
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    • 2021
  • In this paper, we theoretically analyzed the self-alignment/navigation performance in the accelerometer resonance state generated by dither motion of ring laser gyroscope in LINS and verified it through simulation. As a result of analysis, it is confirmed that the amplitude of the accelerometer measurement amplified in the accelerometer resonance state is decreased in the process of sampling per the navigation calculation period and that frequency is changed by the aliasing effect too. It was also analysed that the attitude error in self-alignment is determined by the amplitude/frequency of the accelerometer measurement, the gain of the self-alignment loop, and the velocity and position error in the navigation is determined by the amplitude/frequency/phase error of the accelerometer measurement. This analysis and simulation results show that the self-alignment and navigation performance is not be degraded only when the amplification factor of the accelerometer measurement in the accelerometer resonance state is 3 or less

FIS와 신뢰도를 이용한 레이저 내비게이션의 정밀도 향상 (Accuracy Improvement of Laser Navigation System using FIS and Reliability)

  • 정은국;김정민;정경훈;김성신
    • 한국지능시스템학회논문지
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    • 제21권3호
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    • pp.383-388
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    • 2011
  • 본 논문은 FIS(fuzzy inference system)와 신뢰도를 이용한 레이저 내비게이션의 정밀도 향상에 관한 것이다. 레이저 내비게이션은 무선 유도 장치로써 헤드가 $360^{\circ}$ 회전을 하며 벽에 부착된 반사체(reflector)를 읽어 AGV(automatic guided vehicle)의 위치를 측정하는 장치이다. 기존의 대표적인 유도 장치들의 타입은 유선 유도 방식이다. 이들은 정밀도가 매우 높고 반응속도가 빠르기 때문에 대부분의 현장에서는 이들을 채택하고 있다. 하지만, 이들 센서는 바닥 밑 1인치 안에 설치하거나 바닥에 심어야하기 때문에 설치비용은 매우 높고 유지 보수가 어렵다. 이러한 문제를 해결하기 위해서 레이저 내비게이션이 개발되었다. 이것은 바닥 시공 하는 것이 필요 없고 설치비용이 최소화되며 배치(layout) 변경이 쉽다. 하지만 외란에 영향을 많이 받아 데이터의 손실 손상이 크고 반응속도가 느리기 때문에 안전이 최우선인 산업현장에 사용이 어렵다. 이에 본 논문에서는 레이저 내비게이션의 정밀도 향상에 관한 연구를 하였다. 제안된 방법은 레이저 내비게이션의 특성을 분석하여 FIS를 통해 위치측정 정밀도의 신뢰도를 계산한 후에 이를 통해 레이저 내비게이션의 정밀도를 보정하는 방법이다. 본 논문에서는 실험을 위해서 직접 설계한 AGV를 이용하였으며, 레이저 내비게이션의 위치와 레이저 내비게이션의 신뢰도를 통해 보정된 위치를 제안된 방법과 비교 하였다. 실험 결과, FIS를 신뢰도로 보정한 결과가 다른 방법들에 비해 약 50% 성능이 향상됨을 확인하였다.

Laser-based Relative Navigation Using GPS Measurements for Spacecraft Formation Flying

  • Lee, Kwangwon;Oh, Hyungjik;Park, Han-Earl;Park, Sang-Young;Park, Chandeok
    • Journal of Astronomy and Space Sciences
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    • 제32권4호
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    • pp.387-393
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    • 2015
  • This study presents a precise relative navigation algorithm using both laser and Global Positioning System (GPS) measurements in real time. The measurement model of the navigation algorithm between two spacecraft is comprised of relative distances measured by laser instruments and single differences of GPS pseudo-range measurements in spherical coordinates. Based on the measurement model, the Extended Kalman Filter (EKF) is applied to smooth the pseudo-range measurements and to obtain the relative navigation solution. While the navigation algorithm using only laser measurements might become inaccurate because of the limited accuracy of spacecraft attitude estimation when the distance between spacecraft is rather large, the proposed approach is able to provide an accurate solution even in such cases by employing the smoothed GPS pseudo-range measurements. Numerical simulations demonstrate that the errors of the proposed algorithm are reduced by more than about 12% compared to those of an algorithm using only laser measurements, as the accuracy of angular measurements is greater than $0.001^{\circ}$ at relative distances greater than 30 km.

광궤도를 이용한 이동로봇의 절대위치 보정 시스템 (Absolute Positioning System of Mobile Robot using Light Navigation Path)

  • 박용택;정효용;국금환
    • 한국정밀공학회지
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    • 제20권10호
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    • pp.141-147
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    • 2003
  • This paper represents an absolute positioning system using a light navigation path for mobile robot. The absolute positioning system is composed of the projector unit which generates a laser beam using laser diode and mobile robot with the optical detector which has some optical sensors. The projector unit is fixed over the navigating plane of mobile robot to generate the light navigation path, and the optical detector located upper part of mobile robot detects the generated laser beam from the projector. The navigation of mobile robot is controlled by the micro-processor which compares the detected present position from the detector with the previously programmed navigation path. And experimental results show that our sensor system can be used for the absolute positioning system of the mobile robot.

회전 Laser 슬릿 빔을 이용한 AGV의 위치 및 자세의 검출 (Detection of AGV's position and orientation using laser slit beam)

  • 박건국;김선호;박경택;안중환
    • 한국항해항만학회:학술대회논문집
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    • 한국항해항만학회 2000년도 추계학술대회논문집
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    • pp.219-225
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    • 2000
  • The major movement block of the containers have range between apron and designation points on yard in container terminal. The yard tractor operated by human takes charge of its movement in conventional container terminal. In automated container terminal, AGV(Automated Guided Vehicle) has charge of the yard tractor's role and the navigation path is ordered from upper level control system. The automated container terminal facilities must have the docking system to guide landing line to have high speed travelling and precision positioning. The general method for docking system uses the vision system with CCD camera, infra red, and laser. This paper describes the detection of AGV's position and orientation using laser slit beam to develop docking system.

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KUVE (KIST 무인 주행 전기 자동차)의 자율 주행 (Autonomous Navigation of KUVE (KIST Unmanned Vehicle Electric))

  • 전창묵;서승범;이상훈;노치원;강성철;강연식
    • 제어로봇시스템학회논문지
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    • 제16권7호
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    • pp.617-624
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    • 2010
  • This article describes the system architecture of KUVE (KIST Unmanned Vehicle Electric) and unmanned autonomous navigation of it in KIST. KUVE, which is an electric light-duty vehicle, is equipped with two laser range finders, a vision camera, a differential GPS system, an inertial measurement unit, odometers, and control computers for autonomous navigation. KUVE estimates and tracks the boundary of road such as curb and line using a laser range finder and a vision camera. It follows predetermined trajectory if there is no detectable boundary of road using the DGPS, IMU, and odometers. KUVE has over 80% of success rate of autonomous navigation in KIST.