• Title/Summary/Keyword: Navigation Radar

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Design of Small Optical Tracker for Use in the Proving Ground (시험장 환경에 적합한 소형 광학추적기 설계)

  • Park, Sanghyun
    • Journal of Advanced Navigation Technology
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    • v.24 no.3
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    • pp.224-231
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    • 2020
  • An optical tracking plays an important role for measurement operation, as it is responsible for low altitude measurements that are difficult to obtain with radar systems. Since the existing optical tracking systems have not been developed in the proving ground itself so far, it is difficult to modify them to fit the environment of the proving ground. Also, they are designed as a vehicle-mounted type, so there is a limitation in selecting an optimal site. The in-house developed small optical tracking system is designed with a simple configuration to overcome these shortcomings and makes it possible for operators to operate the system at any place in the proving ground. In addition, there has been a need of developing small optical trackers by ourselves to be prepared for future research so that artificial intelligence (AI) can be applied to the optical tracking systems. In this paper, we described the design concept of the small optical tracker, the configuration of the components to implement the basic tracking function, and showed the results of the simulation to set the configuration of the equipment according to the characteristics of the flight targets.

Analysis of Flight Trajectory Characteristics of Ballistic Missiles Considering Effects of Drag Forces (항력을 고려한 탄도미사일 비행궤적 특성 해석)

  • Kim, Jiwon;Kwon, Yong Soo
    • Journal of Advanced Navigation Technology
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    • v.20 no.2
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    • pp.134-140
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    • 2016
  • This paper analyzed flight trajectory characteristics of ballistic missiles considering effects of drag forces. It is difficult to intercept ballistic missiles which fly over atmosphere with supersonic speeds and small radar cross section (RCS). In particular, the velocities in the phases of boost and terminal are changed significantly due to the steep variation of the drag force. Therefore, in order to build up a successful ballistic missile defense systems, the effects of the drag forces should be considered in the analysis of ballistic missile trajectory characteristics. In this point of view, this work analyzed the effects of drag forces and derived the flight trajectory characteristics of Scud B, C and Nodong missiles. Model of the ballistic missile flight trajectory is considered the effects of Coriolis and centrifugal forces, and specifications of the missiles are open sources.

Detection Performance Comparison of ADS-B and TCAS Using Simulation (시뮬레이션을 활용한 ADS-B와 TCAS의 탐지 성능 비교)

  • So, Jun-Soo;KU, SungKwan;Hong, Gyo-young
    • Journal of Advanced Navigation Technology
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    • v.19 no.6
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    • pp.465-472
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    • 2015
  • In order to improve the performance of TCAS it should improve the performance of the sensor, which transmits a variety of information. In this paper, To improve the performance of the existing radar sensors such as being used in behalf of the next generation air traffic control system, ads-b the applied. In addition, ADS-B in a high precision by using information from the correction GPS system, SBAS assume would be able to apply an improved location accuracy for TCAS and analyzed TCAS and ADS-B. Played the simulation results, TCAS equipment receives the help of these ADS-B can calculate a CPA to determine the position of the aircraft in advance, and it was confirmed that it is possible to reduce the unnecessary RA operation, also, the pilot reduction and the workload, it has advantages such as fuel consumption and time associated with the reduced operation unnecessary RA was confirmed.

Analysis & investigation of EMI dispersion for protection aviation frequency (항공주파수 보호를 위한 전자파방해(EMI)분포조사 및 분석)

  • Park, Duck-Je
    • Journal of Advanced Navigation Technology
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    • v.15 no.5
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    • pp.714-721
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    • 2011
  • In this paper, developing management programs for EMI tracking can navigate the site quickly and solve EMI tracking cause and location to use materials such as analysis of air accidents, EMI site location data of 1000 RF companys, radio wave spectrum analysis and audio data. these data are databased and used comparable data. Also, EMI has been prevented by establishing continuous monitoring system through a 24-hour surveillance. Therefore we were able to provide high quality air waves in order to prevent aircraft accidents. In addition, radar control staff of Korea Airports Corporation against passenger aircraft that will prevent the worst aircraft accident have been established based to continue periodic aviation frequency protection and Portable Electronic Devices(PED) on board aircraft to prevent the culture of safety campaign.

Case Study of Oil Spill Monitoring Caused by Maritime Casualties Using Satellite Data in 2014 (해양사고에 의한 유출유 모니터링 사례 소개와 향후 방향)

  • Yang, Chan-Su
    • Proceedings of the Korean Institute of Navigation and Port Research Conference
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    • 2014.06a
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    • pp.79-80
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    • 2014
  • Most of marine pollution have been occurred by oil spill accidents resulted from ship accidents in South Korea. This year there were two large oil spill accidents: the Yeosu Oil Spill Accident (2014.01.31.(Fri.) 09:35 LT) and the Captain Vangelis L. Oil Spill Accident (2014.02.15.(Sat.) 14:00 LT). In general, Synthetic Aperture Radar (SAR) is used in monitoring and detection of oil dumping and spilled oils by accident at sea. Therefore it is expected that KOMPSAT-5, launched successfully last year, will take part in that mission during a normal operation mode. After the two accidents, high spatial resolution optical satellite data including KOMPSAT-3 were acquired February 2 and 14, 2014. In this presentation, we analyzed optical properties of spilled oils from optical satellite imagery to estimate the spilled area and the volume at each region. Finally, a satellite application planning for ocean surveillance in South Korea will be presented.

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Design and Implementation of Automatic Dependent Surveillance - Broadcast Server System (ADS-B 서버 시스템의 설계 및 구현)

  • Cho, Taehwan;Kim, Kanghee;Kim, Jinhyuk;Choi, Sangbang
    • Journal of Advanced Navigation Technology
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    • v.19 no.3
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    • pp.182-191
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    • 2015
  • The automatic dependent surveillance - broadcast (ADS-B) system which is a core system of aviation system block upgrade is designed and implemented. The ADS-B system consists of the 4 blocks and 10 units, and filtering algorithm is applied to the implemented ADS-B system. To evaluate a performance of the implemented ADS-B system, real aircraft position data is used and compared reliable radar data. The comparison results show that average position difference of 99.57 m. In addition, comparisons of aircraft position data between the implemented ADS-B system employing filtering algorithm and the conventional ADS-B system under various situations are carried out, such as aircraft turning, taking off, landing, and cruising. The comparison results show that average position difference of 8.02 m.

Analysis for FOD Automatic Detection System (FOD 자동탐지시스템 요구사항 분석)

  • Kim, Sung-Hoon;Park, Myoung-Kyu;Hong, Gyo-Young;So, Jun-Soo;Kim, Sang-kwon;Kim, Uri-Eol
    • Journal of Advanced Navigation Technology
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    • v.20 no.3
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    • pp.210-217
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    • 2016
  • Damage caused by FOD which is a foreign substance at the movement area in airports around the world has reached 200 million every year. In 2000, the casualties occurred 133 people at charles de gaulle airport due to FOD. The occurrence of damage by FOD has continuously influenced in domestic also it makes equipment repair indirectly or directly. Accordingly, One of the solutions to the problem is the development of FOD automatic detection system. That is ongoing for plane movement area in airport. As the analyzed result, the military airport prefered mobile type and the civil airport prefered fixed type due to the characteristics of the operating type. In this paper, we analyzed the minimum performance specifications meeting the domestic requirements by investigating military and private FOD detection systems.

Estimating Maintenance Cost of RAPCON at Air Force Base (비행기지 RAPCON 유지보수비용 추정)

  • Bang, Jang-Kyu;Lee, Gun-Young
    • Journal of Advanced Navigation Technology
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    • v.20 no.6
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    • pp.511-518
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    • 2016
  • RAPCON non only controls landing/take-off procedures but also approaching air traffics within 60-70 NM range of air force base. This paper, first of all, tries to research the failure rate per operation hours, mean time between failure (MTBF) of RAPCON according to six blocks such as interrogator, receiver, power unit, display unit, data process unit and antenna. In addition, this paper estimates the maintenance cost over next 10 months based on 50 monthly maintenance cost data. Considering the maintenance cost data from RAPCON which has been used over designed service life span, it is no doubt the forecasted data proved the monthly cost would go up incrementally during the rest of economic life of the facility. Such research result is also proven to be the same with the result of bathtub curve data during operating life.

Frequency-Shifting Digital Demodulator by Bandpass Sampling (대역통과 샘플링을 이용한 주파수 천이 디지털 복조 시스템)

  • Moon, Sung-Bin;Kim, Sae-Yeon;Jung, Shin-Chul;Lee, Byung-Sub
    • Journal of Advanced Navigation Technology
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    • v.4 no.1
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    • pp.36-44
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    • 2000
  • A frequency-shifting technique that uses a digital filter in order to interpolate a bandpass-sampled signal at a low-pass position is investigated. The discussion focuses on the derivation of the required digital filter. It is shown that second-order bandpass sampling offers more flexibility than first-order bandpass sampling in the sense of sampling frequency choice. It is also shown that the well-known quadrature-sampling method for frequency-shifting is a special case of the general second-order sampling technique. The advantages of the mixer-free digital quadrature demodulations are increased flexibility for sampling frequency choice and high precision for I/Q component extraction, and this type of modulation can be applied for modern radar signal processing with high performance.

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Pulse Position Determination using Adaptive Threshold Detector (Adaptive Threshold Detector를 이용한 펄스 위치 계산)

  • Chagn, Jae-won;Lee, Sang Jeong
    • Journal of Advanced Navigation Technology
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    • v.21 no.2
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    • pp.163-170
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    • 2017
  • MLAT which is an independent cooperative surveillance system is applied to increase the positon resoultin of secondary survelliance radar. MLAT uses the hyperboic or hyperboloid position mesurement algorithm. Central processing unit of MLAT calculates target position using time difference of arrival (TDOA) which can be solved from time of arrival (TOA) information of each receivers (at least 4 receivers). To increase position resolution of MLAT which use TDOA, TOA which is transfer time from tranmitter to receiver shold be calculated with precision time resolution in receiver. This paper explained the MLAT system briefly and explained ATD which is one of means of calcuating pulse position. ATD is applied to solve the deviation of pulse position due to different amplitude of signals in mulitiple receivers. In this paper, to analysis the performance of ATD, the simulation result of LAS and CDS was compared with the simulation result of basic threshold method.