• 제목/요약/키워드: Integrated navigation

검색결과 698건 처리시간 0.034초

일반공산비 기법을 이용한 INS/GPS 통합시스템의 고장 검출 및 격리 (Fault Detection and Isolation of Integrated Inertial/Satellite Navigation Systems Using the Generalized Likelihood Ratio Test)

  • 신정훈;임유철;유준
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2000년도 제15차 학술회의논문집
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    • pp.55-55
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    • 2000
  • This paper presents a fault detection and isolation(FDI) method based on Ceneralized Likelihood Ratio(GLR) test for the tightly coupled INS/GPS. State and measurement GLR tests detect INS or GPS fault. Once the fault is detected, Multi-hypothesized GLR scheme performs the fault isolation between INS and GPS and find which satellite malfunctions. Simulation results show that the GLR method is effective enough to detect and isolate a fault of the integrated navigation system.

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소형 통합형 비행조종컴퓨터 개발 (Development of the compact Integrated Flight Control Computer)

  • 장성호;구삼옥;박주원
    • 항공우주시스템공학회지
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    • 제2권1호
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    • pp.17-21
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    • 2008
  • A compact, light-weight, integrated flight control computer(IFCC) for small unmanned autonomous vehicles is developed. Its design objective is to produce an all in one avionics system which includes the navigation sensor, data link, attitude sensors and air data sensors. The initial phase of ground and flight tests are performed to verify the prototype IFCC, showing promising results. The high potential of its application is expected.

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선박의 항해중 종합내항성능지표에 관한 연구 (A Study of the Integrated Seakeeping Performance Index in Seaways)

  • 김순갑;공길영
    • 한국항해항만학회:학술대회논문집
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    • 한국항해항만학회 1997년도 춘계학술발표회 논문집
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    • pp.5-16
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    • 1997
  • This paper presented a method of evaluting navigational safety of a ship by means of the integrated seakeeping performance index(ISPI). The ISPI is defined by measuring only any one factor through the medium of relative dangerousness of the other factors for evaluating seakeeping performance. This evaluation method can be applied to the ships for any types and loading conditions. In developing the practical evaluation system of navigational safety. it is expected to be useful for developing the optimum type of ship by applying at the initial design phase.

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Research on Navigation-aids Information System

  • Zhang, Xing-Gu;Peng, Guo-Jun;Xiang, Lu;Chen, Xin
    • 한국항해항만학회:학술대회논문집
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    • 한국항해항만학회 2006년도 Asia Navigation Conference
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    • pp.56-62
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    • 2006
  • This thesis researches on the application of computer, modern communication, GIS, GPS, AIS and World-Wide-Web in the field of navigation-aids information system, and has realized an integrated system consisted of navigation-aids information GIS platform, navigation-aids monitoring system and navigation-aids information distribution system. This system has strong integration capability, and has realized navigation-aids information distribution based on WEBGIS at the first time. It strongly promotes navigation-aids daily management and maintenance, and this system provides technique guarantee fur ships and marine departments to acquire navigation-aids information in time, by rule and line expediently.

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속도 측정치를 활용한 GPS/INS 통합 항법의 Lever arm 오차 보상 (Lever Arm Error Compensation of GPS/INS Integrated Navigation by Velocity Measurements)

  • 박제두;김민우;김희성;이제영;이형근
    • 한국항공우주학회지
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    • 제41권6호
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    • pp.481-487
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    • 2013
  • GPS/INS 항법시스템의 설치에 있어서 대다수의 경우 GPS 수신기 안테나는 차량의 외부에 설치하게 되고 IMU는 내부에 설치하게 된다. Lever Arm 오차는 이와 같이 센서의 장착 위치 차이로 인하여 발생하는 구조적인 오차에 해당한다. Lever Arm 오차는 항법성능에 직접적으로 영향을 주기 때문에 적절한 보상이 반드시 필요하다. 본 논문에서는 GPS와 INS의 속도 측정치를 활용하여 임의의 위치에 장착된 두 센서의 Lever Arm 오차를 효과적으로 추정하고 보상하는 방식을 제안하였다. 실험을 통해 제안한 알고리즘의 타당성을 검증하였으며, 항체의 회전운동 구간에서 Lever Arm 오차 보상이 특히 중요함을 보였다.

$H_{\infty}$ filter for flexure deformation and lever arm effect compensation in M/S INS integration

  • Liu, Xixiang;Xu, Xiaosu;Wang, Lihui;Li, Yinyin;Liu, Yiting
    • International Journal of Naval Architecture and Ocean Engineering
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    • 제6권3호
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    • pp.626-637
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    • 2014
  • On ship, especially on large ship, the flexure deformation between Master (M)/Slave (S) Inertial Navigation System (INS) is a key factor which determines the accuracy of the integrated system of M/S INS. In engineering this flexure deformation will be increased with the added ship size. In the M/S INS integrated system, the attitude error between MINS and SINS cannot really reflect the misalignment angle change of SINS due to the flexure deformation. At the same time, the flexure deformation will bring the change of the lever arm size, which further induces the uncertainty of lever arm velocity, resulting in the velocity matching error. To solve this problem, a $H_{\infty}$ algorithm is proposed, in which the attitude and velocity matching error caused by deformation is considered as measurement noise with limited energy, and measurement noise will be restrained by the robustness of $H_{\infty}$ filter. Based on the classical "attitude plus velocity" matching method, the progress of M/S INS information fusion is simulated and compared by using three kinds of schemes, which are known and unknown flexure deformation with standard Kalman filter, and unknown flexure deformation with $H_{\infty}$ filter, respectively. Simulation results indicate that $H_{\infty}$ filter can effectively improve the accuracy of information fusion when flexure deformation is unknown but non-ignorable.

디지털 선박의 구현방안 (The method for the development of digital-ship)

  • 박종원;임용곤;전동욱;배진호
    • 한국정보통신학회:학술대회논문집
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    • 한국해양정보통신학회 2001년도 추계종합학술대회
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    • pp.745-748
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    • 2001
  • 디지털 선박은 자율운항 제어 시스템(Intelligent Navigation System), 선박자동식별 시스템(Automatic Identification System), 위성통신망 원격제어 시스템(Integrated Maritime Information Technology)을 기반의 One-man Bridge 시스템을 갖는 차세대 선박을 나타낸다 INS 시스템에서는 선박의 항해와 관련된 기능을 수행하며, 최적항로 계획, 좌초 및 충돌방지 기법, 경제적 운항, 엔진통합제어, 내항성 성능평가 등의 기능이 디지털 GIS(Geographic Information System) 기반의 환경에서 제공된다. AIS 시스템은 선박과 선박간 또는 선박과 관제소간에 선박의 항해 관련 정보를 주기적으로 전송하여 충돌 방지를 기능을 제공하며, IMIT 시스템은 선박내의 통합 플랫폼을 제공하여 선내 네트워크 통합 솔루션을 제공한다. 또한, IMIT 시스템은 위성통신(INMARSAT, OrbComm, 해양관측위성)을 통해 선박과 관제소와의 데이터 송수신을 지원하여, 관제소에서 선박의 항해 상태를 감시하고 선박에 해양 환경정보, 조선소에서의 선박관련 정보 등을 제공하는 기능을 갖는다. 본 논문에서는 디지털 선박의 전체적인 시스템 구현방안과 세부 시스템별 구현방안에 대해 소개하며, 디지털-lT 기반의 차세대 선박에 대한 방향을 제시하도록 한다.

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Real Time Motion Processing for Autonomous Navigation

  • Kolodko, J.;Vlacic, L.
    • International Journal of Control, Automation, and Systems
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    • 제1권1호
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    • pp.156-161
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    • 2003
  • An overview of our approach to autonomous navigation is presented showing how motion information can be integrated into existing navigation schemes. Particular attention is given to our short range motion estimation scheme which utilises a number of unique assumptions regarding the nature of the visual environment allowing a direct fusion of visual and range information. Graduated non-convexity is used to solve the resulting non-convex minimisation problem. Experimental results show the advantages of our fusion technique.

Study on the compensation algorithm for inertial navigation system

  • Kim Hwan-Seong;NGUYEN DuyAnh
    • 한국항해항만학회:학술대회논문집
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    • 한국항해항만학회 2005년도 추계학술대회 논문집
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    • pp.47-52
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    • 2005
  • This paper describes how a relatively compensate the error of position by using low cost Inertial Measurement Unit (IMU) has been evaluated and compared with the well established method based on a Kalman Filter(KF). The compensation algorithm by using IMU have been applied to the problem of integrating information from an Inertial Navigation System (INS). The KF is to estimate and compensate the errors of an INS by using the integrated INS velocity and position. We verify the proposed algorithm by simulation results.

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무인자율수중운동체의 보정항법을 위한 축소된 오차 모델 (Reduced Error Model for Integrated Navigation of Unmanned Autonomous Underwater Vehicle)

  • 박용곤;강철우;이달호;박찬국
    • 제어로봇시스템학회논문지
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    • 제20권5호
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    • pp.584-591
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    • 2014
  • This paper presents a novel aided navigation method for AUV (Autonomous Underwater Vehicles). The navigation system for AUV includes several sensors such as IMU (Inertial Measurement Unit), DVL (Doppler Velocity Log) and depth sensor. In general, the $13^{th}$ order INS error model, which includes depth error, velocity error, attitude error, and the accelerometer and gyroscope biases as state variables is used with measurements from DVL and depth sensors. However, the model may degrade the estimation performance of the heading state. Therefore, the $11^{th}$ INS error model is proposed. Its validity is verified by using a degree of observability and analyzing steady state error. The performance of the proposed model is shown by the computer simulation. The results show that the performance of the reduced $11^{th}$ order error model is better than that of the conventional $13^{th}$ order error model.