• 제목/요약/키워드: Space Navigation

검색결과 1,001건 처리시간 0.038초

Development of a Combined GPS/GLONASS PPP Method

  • Choi, Byung-Kyu;Roh, Kyoung-Min;Lee, Sang Jeong
    • Journal of Positioning, Navigation, and Timing
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    • 제3권1호
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    • pp.31-36
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    • 2014
  • Precise Point Positioning (PPP) is a stand-alone precise positioning approach. As the quality of satellite orbit and clock products from analysis centers has been improved, PPP can provide more precise positioning accuracy and reliability. A combined use of Global Positioning System (GPS) and Global Orbiting Navigation Satellite System (GLONASS) in PPP is now available. In this paper, we explained about an approach for combined GPS and GLONASS PPP measurement processing, and validated the performance through the comparison with GPS-only PPP results. We also used the measurement obtained from the GRAS reference station for the performance validation. As a result, we found that the combined GPS/GLONASS PPP can yield a more precise positioning than the GPS-only PPP.

Positioning Precision Improvement of Multi-GNSS Kinematic PPP Using WMN Method

  • Choi, Byung-Kyu;Yoon, Ha Su;Lee, Sang Jeong
    • Journal of Positioning, Navigation, and Timing
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    • 제6권4호
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    • pp.205-210
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    • 2017
  • Multi-Global Navigation Satellite System (GNSS) can significantly improve the positioning accuracy and convergence speed. The reliability and availability of multi-GNSS precise point positioning (PPP) is steadily increasing with the rapid development of GNSS satellites. In this study, multi-GNSS PPP analysis is performed to compare the positioning precision by processing the observations from different GNSS systems (GPS, GLONASS, Galileo and BeiDou). To improve the positioning performance of the multi-GNSS PPP, we employed the weighed measurement noise (WMN) method. After applying WMN method to multi-GNSS PPP, positioning precision is improved by approximately 26.3% compared to the GPS only solutions, and by approximately 9.1% compared to combined GPS, GLONASS, and Galileo PPP.

Accuracy Improvement of Multi-GNSS Kinematic PPP with EKF Smoother

  • Choi, Byung-Kyu;Sohn, Dong-Hyo;Lee, Sang Jeong
    • Journal of Positioning, Navigation, and Timing
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    • 제10권2호
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    • pp.83-89
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    • 2021
  • The extended Kalman filter (EKF) is widely used for global navigation satellite system (GNSS) applications. It is difficult to obtain precise positions with an EKF one-way (forward or backward) filter. In this paper, we propose an EKF smoother to improve the positioning accuracy by integrating forward and backward filters. For the EKF smoother experiment, we performed PPP using GNSS data received at the DAEJ reference station for a month. The effectiveness of the proposed approach is validated with multi-GNSS kinematic PPP experiments. The EKF smoother showed 35%, 6%, and 22% improvement in east, north, and up directions, respectively. In addition, accurate tropospheric zenith total delay (ZTD) values were calculated by a smoother. Therefore, the results from EKF smoother demonstrate that better accuracy of position can be achieved.

Efforts against Cybersecurity Attack of Space Systems

  • Jin-Keun Hong
    • Journal of Positioning, Navigation, and Timing
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    • 제12권4호
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    • pp.437-445
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    • 2023
  • A space system refers to a network of sensors, ground systems, and space-craft operating in space. The security of space systems relies on information systems and networks that support the design, launch, and operation of space missions. Characteristics of space operations, including command and control (C2) between space-craft (including satellites) and ground communication, also depend on wireless frequency and communication channels. Attackers can potentially engage in malicious activities such as destruction, disruption, and degradation of systems, networks, communication channels, and space operations. These malicious cyber activities include sensor spoofing, system damage, denial of service attacks, jamming of unauthorized commands, and injection of malicious code. Such activities ultimately lead to a decrease in the lifespan and functionality of space systems, and may result in damage to space-craft and, lead to loss of control. The Cybersecurity Adversarial Tactics, Techniques, and Common Knowledge (ATT&CK) matrix, proposed by Massachusetts Institute of Technology Research and Engineering (MITRE), consists of the following stages: Reconnaissance, Resource Development, Initial Access, Execution, Persistence, Privilege Escalation, Defense Evasion, Credential Access, Discovery, Lateral Movement, Collection, Command & Control, Exfiltration, and Impact. This paper identifies cybersecurity activities in space systems and satellite navigation systems through the National Institute of Standards and Technology (NIST)'s standard documents, former U.S. President Trump's executive orders, and presents risk management activities. This paper also explores cybersecurity's tactics attack techniques within the context of space systems (space-craft) by referencing the Sparta ATT&CK Matrix. In this paper, security threats in space systems analyzed, focusing on the cybersecurity attack tactics, techniques, and countermeasures of space-craft presented by Space Attack Research and Tactic Analysis (SPARTA). Through this study, cybersecurity attack tactics, techniques, and countermeasures existing in space-craft are identified, and an understanding of the direction of application in the design and implementation of safe small satellites is provided.

차세대 위성항법체계 갈릴레오 센서스테이션 유치 후보지 전파 수신환경 조사: I. KVN 탐라전파천문대 인근 부지에 대한 2006년 한국천문연구원 조사 결과 (RF ENVIRONMENT TEST ON A PROPOSED SITE FOR THE SENSOR STATION OF THE NEXT GENERATION SATELLITE NAVIGATION SYSTEM, GALILEO: I. THE RESULT OF THE TEST ON THE VICINITY OF KVN TAMLA SITE IN THE YEAR OF 2006 BY KASI)

  • 조중현;제도흥;조성기;최병규;백정호;이대규;정현수;임형철;조정호;이우경;정성욱;박종욱;최남미
    • Journal of Astronomy and Space Sciences
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    • 제25권1호
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    • pp.43-52
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    • 2008
  • 2007년에 Giove-A 실험위성의 항법메시지 송신 시험이 성공적으로 끝마침으로써, 차세대 위성 항법시스템인 갈릴레오 계획이 초기궤도 검증단계를 앞두고 있다. 한국천문연구원의 우주측지연구부와 전파천문연구부는 제주 탐라대학교 내 유치 후보지에 대한 갈릴레오 센서 스테이션 전파 수신환경 공동조사를 2006년 8월 3일부터 5일까지 실시했다. 전계강도 스펙트럼은 전 대역$(800{\sim}2000MHz)$과 내 대역(E5, E6, L1 밴드)에 대해서 24시간 주파수 영역 관측을 했다. 이 단계에서 관측된 강한 내 대역 간섭 신호에 대해서 시간영역 분석을 했다.

3차원 가상공간에서의 상호작용적 네비게이션 디자인 1부: 기초개념 및 기술 (Interactive Navigation Design in 3-Dimensional Virtual Space Part I: Basic Concepts and Techniques)

  • 김진희
    • 디자인학연구
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    • 제16권3호
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    • pp.71-80
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    • 2003
  • 가상현실 분야는 이제 대중화시대를 맞이하고 있다. 데스크탑 가상현실 산업은 다양한 Web VR 애플리케이션을 중심으로 급속히 성장하고 있는 추세이다. 3차원 가상공간에서 사용자 네비게이션의 수행은 가상의 공간에 설정된 논리적 구조를 인지하고 설정된 상호작용을 이해하며 길을 찾아가는 복잡한 과정이다. 그 것은 사용자가 임으로 설정하는 과정이 아니고 기획단계에서 면밀히 디자인되고 설계된 기술적, 기법적 그리고 개념적 과정인 것이다. 이에 따라 본 논고에서는 3차원 가상공간에서의 상호작용적 네비게이션과 관련된 기술적, 기법적, 그리고 개념적 기초이론들을 총체적으로 고찰하고 있다.

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Space Service Volume Augmented with Korean Positioning System at Geosynchronous Orbit

  • Kim, Gimin;Park, Chandeok;Lim, Deok Won
    • Journal of Positioning, Navigation, and Timing
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    • 제9권4호
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    • pp.327-336
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    • 2020
  • This study presents signal availability of inter-operable global navigation satellite system (multi-GNSS) combined with future Korean Positioning System (KPS), specifically at geosynchronous orbit (GSO). The orbit of KPS, which is currently under conceptual feasibility study, is first introduced, and the grid points for evaluating space service volume (SSV) at GSO are generated. The signal observabilities are evaluated geometrically between those grid points and KPS/GNSS satellites. Then, analyzed are the visibility averaged over time/space and outage time to not access one or four signals. The reduction of maximum outage time induced by KPS are presented with different maximum off-boresight angles depending on L1/E1/B1 and L5/L3/E5a/B2 frequencies. Our numerical analysis shows that the SSV of multi-GNSS combined with KPS provides up to 7 additional signals and could provide continuous observation time (zero outage time) of more than four GNSS or KPS signals for 3.20-14.83% of SSV grid points at GSO. Especially at GSO above North/South America and Atlantic region, the introduction of KPS reduces the outage duration by up to 63 minutes with L1/E1/B1 frequency.

정밀 행성 착륙을 위한 지형 보조 관성 항법 연구 (Terrain Aided Inertial Navigation for Precise Planetary Landing)

  • 정보영;최윤혁;조수장;방효충
    • 한국항공우주학회지
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    • 제38권7호
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    • pp.673-683
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    • 2010
  • 본 논문에서는 정밀 행성 착륙을 위해 광학센서와 관성항법시스템을 이용한 지형보조 관성항법 시스템을 구현하였다. 또한 측정된 지형 데이터와 사전에 탑재한 지형 데이터간의 특징점 추출, 매칭, 추적의 영상 처리 과정을 수행하였고 이를 통해 특징점의 좌표를 추출할 수 있다. 반복 확장칼만필터를 이용한 항법 시스템은 기존 관성 항법 장치의 항법 오차 누적을 보상하여 보다 정밀한 항법 정보를 제공한다. 이는 향후 착륙선의 유도 및 제어 법칙과 결합하여 정밀 행성 착륙을 위한 시스템 구현에 적용이 가능하다.

APPLICABLE TRACKING DATA ARCS FOR NORAD TLE ORBIT DETERMINATION OF THE KOMPSAT-1 SATELLITE USING GPS NAVIGATION SOLUTIONS

  • Lee, Byoung-Sun
    • Journal of Astronomy and Space Sciences
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    • 제22권3호
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    • pp.243-248
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    • 2005
  • NORAD Two Line Element (TLE) is very useful to simplify the ground station antenna pointing and mission operations. When a satellite operations facility has the capability to determine NORAD type TLE which is independent of NORAD, it is important to analyze the applicable tracking data arcs for obtaining the best possible orbit. The applicable tracking data arcs for NORAD independent TLE orbit determination of the KOMPSAT-1 using GPS navigation solutions was analyzed for the best possible orbit determination and propagation results. Data spans of the GPS navigation solutions from 1 day to 5 days were used for TLE orbit determination and the results were used as Initial orbit for SGP4 orbit propagation. The operational orbit determination results using KOMPSAT-1 Mission Analysis and Planning System(MAPS) were used as references for the comparisons. The best-matched orbit determination was obtained when 3 days of GPS navigation solutions were used. The resulting 4 days of orbit propagation results were within 2 km of the KOMPSAI-1 MAPS results.