• Title/Summary/Keyword: s-INS

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Aided Navigation Algorithm for Land Navigation System Using VMS with Indirect Drive Condition (직진성이 보장되지 않는 조건에서 지상항법시스템의 속도계를 이용한 보정항법 알고리즘)

  • Kim, Hyungsoo
    • Journal of Advanced Navigation Technology
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    • v.20 no.4
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    • pp.314-320
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    • 2016
  • Inertial navigation system (INS) has used aided systems and sensors to compensate navigation error. Global navigation satellite system (GNSS), velocity measurement sensor (VMS), and radar are commonly used to aid INS. Land navigation system (LNS) also mainly uses VMS when GNSS cannot be used such as at tunnel or on jammed scenario. A straight drive is required when VMS-aided navigation is used, because there is only speed of straight direction whereas no crossways and vertical directions. In local environment, even an expressway has lack of straight drive which is constraint of VMS-aided navigation algorithm. This paper proposes an enhanced VMS-aided navigation algorithm for LNS with indirect drive by restricting filter update condition. Also, there is a result of vehicle test to prove performance of the proposed algorithm.

Development of Localization Tracking System and User Interface of Guiding Robot for the Visually Impaired (시각장애인 유도 로봇의 자기 위치 추적 시스템 및 사용자 인터페이스 개발)

  • Ryu Je-Goon;Shen Dong-Fan;Kwon Oh-Sang;Kim Nack-Hwan;Lee Sang-Moo;Lee Eung-Hyuk;Hong Seung-Hong
    • The KIPS Transactions:PartD
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    • v.12D no.3 s.99
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    • pp.481-492
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    • 2005
  • To guide the guiding robot for the visually impaired carefully, the digital map to be used to search a path must be detailed and has some information about dangerous spots. It also has to search not only safe but also short path through the position data by GPS and INS sensors. In this paper, as the difference of the ability that the visually unpaired can recognize, we have developed the localization tracking system so that it can make a movement path and verify position information, and the global navigation system for the visually impaired using the GPS and INS. This system can be used when the visually impaired move short path relatively. We had also verified that the system was able to correct the position as the assistant navigation system of the GPS on the outside.

Design and Implementation of Real-Time Operating System for a GPS Navigation Computer (GPS 항법 컴퓨터를 위한 실시간 운영체제의 설계 및 구현)

  • Bae, Jang-Sik;Song, Dae-Gi;Lee, Cheol-Hun;Song, Ho-Jun
    • The KIPS Transactions:PartA
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    • v.8A no.4
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    • pp.429-438
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    • 2001
  • GPS (Global Positioning System) is the most ideal navigation system which can be used on the earth irrespective of time and weather conditions. GPS has been used for various applications such as construction, survey, environment, communication, intelligent vehicles and airplanes and the needs of GPS are increasing in these days. This paper deals with the design and implementation of the RTOS (Real-Time Operating System) for a GPS navigation computer in the GPS/INS integrated navigation system. The RTOS provides the optimal environment for execution and the base platform to develop GPS application programs. The key facilities supplied by the RTOS developed in this paper are priority-based preemptive scheduling policy, dynamic memory management, intelligent interrupt handling, timers and IPC, etc. We also verify the correct operations of all application tasks of the GPS navigation computer on the RTOS and evaluate the performance by measuring the overhead of using the RTOS services.

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Integrated Navigation System Design of Electro-Optical Tracking System with Time-delay and Scale Factor Error Compensation

  • Son, Jae Hoon;Choi, Woojin;Oh, Sang Heon;Hwang, Dong-Hwan
    • Journal of Positioning, Navigation, and Timing
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    • v.11 no.2
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    • pp.71-81
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    • 2022
  • In order for electro-optical tracking system (EOTS) to have accurate target coordinate, accurate navigation results are required. If an integrated navigation system is configured using an inertial measurement unit (IMU) of EOTS and the vehicle's navigation results, navigation results with high rate can be obtained. Due to the time-delay of the navigation results of the vehicle in the EOTS and scale factor errors of the EOTS IMU in high-speed and high dynamic operation of the vehicle, it is much more difficult to have accurate navigation results. In this paper, an integrated navigation system of EOTS which compensates time-delay and scale factor error is proposed. The proposed integrated navigation system consists of vehicle's navigation system which provides time-delayed navigation results, an EOTS IMU, an inertial navigation system (INS), an augmented Kalman filter and integration Kalman filter. The augmented Kalman filter outputs navigation results, in which the time-delay of the vehicle's navigation results is compensated. The integration Kalman filter estimates position, velocity, attitude error of the EOTS INS and accelerometer bias, accelerometer scale factor error, gyro bias and gyro scale factor error from the difference between the output of the augmented Kalman filter and the navigation result of the EOTS INS. In order to check performance of the proposed integrated navigation system, simulations for output data of a measurement generator and land vehicle experiments were performed. The performance evaluation results show that the proposed integrated navigation system provides more accurate navigation results.

Measurement Time-Delay Compensation and Initial Attitude Determination of Electro-Optical Tracking System Using Augmented Kalman Filter (Augmented 칼만 필터를 이용한 전자광학 추적 장비의 측정치 시간지연 보상과 초기 자세 결정)

  • Son, Jae Hoon;Choi, Woo Jin;Kim, Sung-Su;Oh, Sang Heon;Lee, Sang Jeong;Hwang, Dong-Hwan
    • Journal of Korea Multimedia Society
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    • v.24 no.12
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    • pp.1589-1597
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    • 2021
  • Due to the low output rate and time delay of vehicle's navigation results, the electro-optical tracking system(EOTS) cannot estimate accurate target positions. If an inertial measurement unit(IMU) is additionally mounted into the EOTS and inertial navigation system(INS) is constructed, the high navigation output rate can be obtained. And the time-delay can be compensated by using the augmented Kalman filter. An accurate initial attitude is required in order to have accurate navigation outputs. In this paper, an attitude determination algorithm is proposed using the augmented Kalman filter in order to compensate measurement delay of the EOTS and have accurate initial attitude. The proposed initial attitude determination algorithm consists of an augmented Kalman filter, an INS, and an integrated Kalman filter. The augmented Kalman filter compensates the time-delay of the vehicle's navigation results and the integrated Kalman filter estimates the navigation error of the INS. In order to evaluate performance of the proposed algorithm, vehicle's navigation outputs and IMU measurements were generated using sensors' model-based measurement generator and initial attitude estimation errors of the proposed algorithm and the conventional algorithm without the augmented Kalman filter were compared for the generated measurements. The evaluation results show that the proposed algorithm has better accuracy.

Four Dammarane Triterpenes and Their Inhibitory Properties Against Eight Receptor Tyrosine Kinases

  • Heliawati, Leny;Khatimah, Husnul;Hermawati, Elvira;Syah, Yana Maolana
    • Natural Product Sciences
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    • v.26 no.4
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    • pp.345-350
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    • 2020
  • In recent years, tyrosine kinases (TKs) have been the target to combat cancers, and most of the developed inhibitors are of synthetic origin. Natural compounds that have the properties as the TK's inhibitors are very limited. This paper described the isolation of a new dammarane triterpene from the tree bark of Sandoricum koetjape, along with three known related dammaranes from the damar resin of Shorea javanica, as well as their inhibitory properties against eight receptor TKs (RTKs: EGFR, HER2, HER4, IGF1R, InsR, KDR, PDGFRα, and PDGFRβ). Based on the NMR and mass spectral data the new compound was identified as (12β,20S)-12,20-dihydroxy-3,4-seco-dammaran-4,24-dien-3-oic acid (12β-hydroxydammarenolic acid) (1), while the three known compounds were identified as (20S)-20-hydroxy-3,4-seco-dammaran-4,24-dien-3-oic acid (dammarenolic acid) (2), (3β,20S)-3,20-dihydroxydammaran-24-ene (3), and (20S)-3-oxo-20-hydroxydammaran-24-ene (4). The tyrosine kinase assay of the four compounds resulted only 1 and 2 at concentration of 10 μM that had weak activity against EGFR and InsR, with their % inhibitory were 30%, 27% (1), 45%, and 32% (2), respectively. The results suggested that the presence of a linear carboxylic acid group in both compounds could be of significance to the inhibitory properties against the two RTKs.

Packet Communication Services in Japan (일본 NTT의 패킷 통신서비스 현황)

  • Oh, H.S.;Kang, S.J.
    • Electronics and Telecommunications Trends
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    • v.8 no.3
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    • pp.163-183
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    • 1993
  • NTT는 1980년에 DDX-P 패킷통신서비스를 개시하여 현재 DDX-TP, DDX-TP 및 INS-P의 3종류의 서비스를 제공하고 있다. 본 고는 NTT의 패킷통신망 구조, 기능 및 싱호통신 등 NTT 패킷통신서비스 전반적인 면과 이를 이용한 사례를 분석한 결과이다.

Performance Analysis of Navigation System for Guidance and Control of High Speed Underwater Vehicle System (고속 수중운동체 정밀 유도제어를 위한 항법성능 분석)

  • Hong, Sung-Pyo;Han, Yong-Su
    • Journal of the Korea Institute of Information and Communication Engineering
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    • v.17 no.9
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    • pp.2227-2232
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    • 2013
  • To obtain the system requirement specification in the beginning of the precision guidance system development, the effectiveness and reliability analysis for the system are necessary. The main purpose of this research is to obtain the system requirement specification for the high speed unmanned underwater vehicles by carrying out the effectiveness analysis using the modeling and simulation scheme. The effectiveness is position error for target position. Reaching accuracy is expected to be affected by the navigation sensor parameter. Assume that the navigation sensors that is consist of inertial navigation system(INS) and doppler velocity log(DVL) is the parameter. To analyze the effectiveness of each parameter, Monte-Carlo numerical simulation is performed in this research. The effectiveness analysis is carried out using circular error probability(CEP) and variance analyze scheme. Considering the cost function, the specification of the navigation sensor is provided. The cost function is consist of the INS and DVL specification and the price of those sensors.