• Title/Summary/Keyword: Integrated navigation

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A Study on the Applications of GPS/Pseudolite Navigation System (GPS/의사위성의 통합 항법에 대한 응용 연구)

  • Lee Taik-Jin;Kim kang-Ho;So Hyung-Min;Kee Chang-Don;Noh Kwang-Hyun;Lee Ki-Duk
    • Journal of Institute of Control, Robotics and Systems
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    • v.12 no.8
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    • pp.729-738
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    • 2006
  • In recent days, navigation technology becomes more important as location based service (LBS) such as E911 and telematics are considered as attractive business fields. Commercial LBS requires that navigation system should be inexpensive and available anytime and anywhere - indoors and outdoors. If we consider these requirements, it is out of question that GPS is the most favorite system in the world. However, GPS has a serious problem. The one is that GPS does not operate indoors well. This is because GPS satellites are about 20,000km above the ground so that indoor signals are too weak to be tracked in GPS receiver. And the other is that vertical accuracy is less than horizontal accuracy, because of GPS satellites' geometry. To solve these problems, many researches have been done around the world since 1990s. This paper is also one of them and we will introduce an excellent solution by use of pseudolite. Pseudolite is a kind of signal generator, which transmits GPS-like signal. So it is same as GPS satellite in ground. In this paper, we will propose the integrated navigation system of GPS and pseudolite and show the flight test results using RC airplane to proof our navigation system. As a result, we could improve the vertical accuracy of airplane into the horizontal accuracy.

Practical Applications Study of the Pseudolite (의사위성 활용방안 연구)

  • Chang, Jae-Won;Kwon, TaeHee;Lee, Sang Jeong
    • Journal of Advanced Navigation Technology
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    • v.8 no.2
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    • pp.129-135
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    • 2004
  • In this paper, the practical applications of the pseudolite are explained with the basic concept of the pseudolite. Many researches have been developed to improve the performance of the GPS. Most of those researches need the extra equipments. But without the extra equipments, the performance of GPS can be improved only with the change in the software in GPS system. In this paper, the pseudolite and the integrated navigation system including GPS as well as pseudolite only with navigation system for the demand of more precise navigation system are introduced. Also, the advantage of the pseudolite is confirmed by some simulations.

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Measurement Delay Error Compensation for GPS/INS Integrated System (GPS/INS 통합시스템의 측정치 시간지연오차 보상)

  • Lyou Joon;Lim You-Chol
    • Journal of the Institute of Electronics Engineers of Korea SC
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    • v.41 no.1
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    • pp.1-8
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    • 2004
  • The INS(Inertial Navigation System) provides high rate position, velocity and attitude data with good short-term stability while the GPS(Global Position System) provides position and velocity data with long-term stability. By integrating the INS with GPS, a navigation system can be achieved to Provide highly accurate navigation Performance. For the best performance, time synchronization of GPS and INS data is very important in GPS/INS integrated system But, it is impossible to synchronize them exactly due to the communication and computation time-delay. In this paper, to reduce the error caused by the measurement time-delay in GPS/INS integrated systems, error compensation methods using separate bias Kalman filter are suggested for both the loosely-coupled and the tightly-coupled GPS/INS integration systems. Linearized error models for the position and velocity matching GPS/INS integrated systems are Int derived by linearizing with respect to its time-delay and augmenting the delay-state into the conventional state equations for each case. And then separate bias Kalman Inter is introduced to estimate the time-delay during only initial navigation stage. The simulation results show that the present method is effective enough resulting in considerably less position error.

Operational Concept for the Software Product Line Framework of Navigation Software (항법소프트웨어 Software Product Line 프레임워크 운영개념)

  • Park, Samjoon;Noh, Sungkyu;Kim, Dohyung;Lee, Sunju;Park, ByungSu;Lee, Inseop
    • KIPS Transactions on Software and Data Engineering
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    • v.10 no.6
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    • pp.201-210
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    • 2021
  • Navigation Software for the various weapon systems has common functionalities which give the possibility of common use among them. SPL(Software Product Line) framework of the navigation software for weapon system refers to developing a standardized navigation software platform from common functionalities of navigation software, managing the standardized navigation software platform, and developing weapon system navigation software such as navigation software for missile, UAV(Unmanned Air Vehicle), submarine, and etc. from the standardized navigation software platform. In this paper, we propose SPL based navigation software development process, Integrated Development Environment and operational concept of SPL framework. The operational concept will be defined by specifying the role of every stake holders and their activity scenario. The Operational concept would be referenced to implement SPL for other domain through using with detail implementation guide.

Design of Navigation System for Low Cost Unmanned Aerial Vehicle (저가형 무인항공기 운용을 위한 항법시스템 설계)

  • Lee, Jang-Ho;Kim, Sung-Pil;Park, Mu-Hyeok;Ahn, Iee-Ki
    • Journal of Advanced Navigation Technology
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    • v.8 no.2
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    • pp.105-111
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    • 2004
  • This paper describes the design of navigation system for an unmanned target drone which is operated by Korean army as for anti-air gun shooting training. Current target drone is operated by pilot control of on-board servo motor via remote control system. Automatic flight control system for the target drone greatly reduces work load of ground pilot and can increase application area of the drone. Most UAVs being operated nowdays use high-priced sensors as AHRS and IMU to measure the attitude, but those are costly. This paper introduces the development of low-cost automatic flight control system with low-cost sensors. The integrated automatic flight control system has been developed by integrating combining power module, switching module, monitoring module and RC receiver as an one module. The performance of navigation for low cost unmanned aerial vehicle, unmanned target drone as our test bed in this paper is verified by both Hardware in the loop simulation(HILS) to test performance of GPS as GPS output frequency high and results of flight test.

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Development of Integrated Navigation Computer for On/Off Line Processing (실시간/후처리 기법을 고려한 복합 항법 컴퓨터 개발)

  • Jin, Yong;Park, Chan-Gook
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.30 no.8
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    • pp.133-140
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    • 2002
  • In this paper, the structure of integrated navigation computer for experiment is proposed. It is designed for considering the real time processing and data storage capacity. It will be used in missile, aircraft, submarine system and experimental vehicle. The I/O device supports IMU, GPS, odometer, altimeter, depth sensor, inclinometer etc. And the main storage device uses the tape device. That can improve the system stability. Therefore it can be used in a high dynamic or shock environment. The embedded linux is used as an Operating System. For the real time capability, sensor data processing and algorithm processing units are seperated. The time synchronization is referenced by IMU data.

Observability Analysis of a Vision-INS Integrated Navigation System Using Landmark (비전센서와 INS 기반의 항법 시스템 구현 시 랜드마크 사용에 따른 가관측성 분석)

  • Won, Dae-Hee;Chun, Se-Bum;Sung, Sang-Kyung;Cho, Jin-Soo;Lee, Young-Jae
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.38 no.3
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    • pp.236-242
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    • 2010
  • A GNSS/INS integration system can not provide navigation solutions if there are no available satellites. To overcome this problem, a vision sensor is integrated with this system. Since generally a vision aided integration system uses only feature point to compute navigation solutions, it has a problem in observability. In this case, additional landmarks, which is priory known points, can improve the observability. In this paper, the observability is evaluated using TOM/SOM matrix and Eigenvalues. There are always the observability problems in the feature-point-only case, but the landmark-use case is fully observable after the $2^{nd}$ update time. Consequently the landmarks ensure full observability, so the system performance can be improved.

Integrated Structural Design of Oceanic Buildings using STEP (STEP을 이용한 해양건축물의 통합구조설계 기법)

  • 송화철
    • Journal of Korean Port Research
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    • v.14 no.1
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    • pp.77-86
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    • 2000
  • The planning process of complex projects in oceanic architectural engineering is characterized by the cooperation of many involved specialists and by a high degree of information exchange. In order to improve the quality of the structural design of oceanic buildings, information of different involved partners in the planning process has to be integrated. This paper aims to introduce a concept of the integrated structural design for the floating-type oceanic building using STEP(Standard for the Exchange of Product Model Data). STEP(ISO 10303) is an international standard for the computer-interpretable representation and exchange of product data and it provides a consistent data exchange format and application interfaces between different application systems. In this paper, the structural design process and information of oceanic buildings is analyzed and product models are preposed fir the exchange of the structural design information between superstructure and floating structure. The entities for calculating wind loads, metacenter and restoring forces are represented by Express. As a case study a floating hotel is applicated to describe the STEP physical file.

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Integrated Indoor Positioning Systems Reflecting Map Information for Location Based Services (위치기반서비스를 위한 지도정보가 반영된 옥내측위통합 시스템)

  • Yim, Jae-Geol;Joo, Jae-Hun;Jeong, Seung-Hwan
    • The Journal of Information Systems
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    • v.17 no.1
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    • pp.131-153
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    • 2008
  • So many location based service systems, including automobile navigation system logistic management, taxi fleet management, and so on, are being used everywhere. However, these are all outdoors. This paper provides a stepping stone for commercial indoor location based services by developing an integrated system of our indoor positioning and map viewer modules. For the indoor positioning, we propose WLAN (Wireless Local Area Network) based EKF (Extended Kalman Filter) which estimates user's current location and tracts user's trace in the sequence of time. Our map viewer renders a map recorded in an Autocad DXF file and provides functions of map manipulation such as zoom-in, zoom-out, and move. We integrate our indoor positioning and map viewer modules and discuss the experimental results of the integrated system.

Development of an INS Integrated Positioning System for Assisting Effective Fire-fighting Activity

  • Suh, Yong-Cheol;Kumagai, Hideo;Konishi, Yusuke;Shibasaki, Ryosuke
    • Proceedings of the KSRS Conference
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    • 2003.11a
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    • pp.946-948
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    • 2003
  • This paper describes the development of an INS (Inertial Navigation System) integrated positioning system, which can monitor and track the firefighter's position for assisting effective fire-fighting activity and rescue services. The INS consists of highly accurate three-axis gyro sensor and three-axis accelerometer. By integrating an INS to positioning system, it is also possible to obtain the information of firefighter's physical state (e.g. standing, collapse and crouch) of posture including velocity. Consequently, this research would obviously make a contribution to effective rescue activities and safety of firefighters. Besides, this paper presents results from field tests conducted at Tokyo University demonstrating its viability and utility. We also summarize the overall system requirements and architecture, and describe the hardware and software used in the prototype system in detail.

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