• Title/Summary/Keyword: MLAT

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Performance analysis for Ground Position Accuracy Test of MLAT (MLAT 지상 위치정확도 시험에 대한 성능 분석)

  • Koo, Bon-soo;Jang, Jae-won;Kim, Woo-riul;Kim, Tae-sik
    • Journal of Advanced Navigation Technology
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    • v.21 no.4
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    • pp.325-331
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    • 2017
  • As a GPS stability problem arises, MLAT system is spotlighted as an alternative technology of ADS-B. MLAT system has a high position accuracy as much as ADS-B. Also, MLAT receives the mode A,C,S, and 1090ES(ADS-B) signals from the mounted aircraft transponder. MLAT receives signals from several receiver units and calculates aircraft positions. MLAT has ADS-B level positioning accurarcy using GPS and can calculate the position information with objects independently. According to global environment changes, Local area multiltilateration(LAM) surveillance system is under development for moving vehicles and aircraft detection in airport. These are still under testing in Tae-an Airfield. In the paper, we analyzed the performance by comparing the calculated position data from MLAT to RTK. In order to confirm the position accuracy of MLAT and the deviation of position data between fixed target and moving target on the ground during the field test in Tae-an Airfield.

다변측정(Multilateration) 항공감시 시스템 기술 동향

  • Kim, Tae-Sik;Jang, Jae-Won
    • The Optical Journal
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    • s.151
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    • pp.46-54
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    • 2014
  • 향후 민간항공분야에서 지상감시 장비로 중요한 역할을 담당할 MLAT을 국내 개발을 위해 세계적인 변화에 대응하고자 항공감시와 관련한 기술현황을 조사하고 MLAT에 대한 기술개발을 추진하고자 이와 관련하여 국내개발방안에 대한 연구를 수행하였다. 항공감시 기술현황과 관련해서는 현재 및 미래에 사용될 항공감시 장비에 대한 기술을 소개와 기술발전 전망을 예측해 보았다. 그리고 MLAT 시스템을 국내개발하기 위해 MLAT 기술을 조사하고 국내개발 시스템에 대한 구성도를 설계하였다. MLAT은 SSR과 같이 독립적으로 표적을 감시할 수 있을 뿐만 아니라 ADS-B정도의 정밀도를 가지고 있어 향후 미래 항공의 주 시스템으로써의 역할을 할 것이다.

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Aircraft Track Estimation Algorithm for MLAT System (MLAT 시스템용 표적 위치추정 알고리즘)

  • Kim, Do-Hoon;Hwang, Kyu-Sung;Ju, MinChul
    • The Journal of Korean Institute of Communications and Information Sciences
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    • v.39A no.2
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    • pp.117-119
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    • 2014
  • In this paper, we shows the simulation result of estimation algorithm for aircraft track which is core engine in MLAT system. The simulation result for 3D position estimation by Chan algorithm based on TDOA and Kalman filter shows that the performance satisfies the requirements of EUROCAE ED-117 over AWGN channel.

Alternative Positioning, Navigation and Timing Using Multilateration in a Terminal Control Area (접근관제구역에서 다변측정감시시스템을 이용한 대안항법 방안 연구)

  • Jo, Sanghoon;Kang, Ja-young
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.23 no.3
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    • pp.35-41
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    • 2015
  • Multilateration(MLAT) is commonly used in civil and military surveillance applications to accurately locate an aircraft, vehicle or stationary emitter. MLAT calculates the TDOA of signals by transmitted aircraft and determines the aircraft's location. With more than four receivers it is possible to estimate the 3D position of the aircraft by calculating the intersection of the resulting hyperbolas and the system integrity. In this study, our objectives are to apply MLAT technique to Jeju terminal control area and to propose a MLAT receiver network to properly estimate the positions of aircraft approaching this area. Based on computer simulations, we determine locations of ground receivers in Jeju terminal control area, calculate estimated position errors of the aircraft with respect to the selected receiver networks, and find the best receiver network with the least position error.

An Efficient Information Fusion Method for Air Surveillance Systems (항공감시시스템을 위한 효율적인 정보융합 기법)

  • Cho, Taehwan;Oh, Semyoung;Lee, Gil-Young
    • Journal of Advanced Navigation Technology
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    • v.20 no.3
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    • pp.203-209
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    • 2016
  • Among the various fields in the communications, navigation, and surveillance/air traffic management (CNS/ATM) scheme, the surveillance field, which includes an automatic dependent surveillance - broadcast (ADS-B) system and a multilateration (MLAT) system, is implemented using satellite and digital communications technology. These systems provide better performance than radar, but still incur position error. To reduce the error, we propose an efficient information fusion method called the reweighted convex combination method for ADS-B and MLAT systems. The reweighted convex combination method improves aircraft tracking performance compared to the original convex combination method by readjusting the weights given to these systems. In this paper, we prove that the reweighted convex combination method always provides better performance than the original convex combination method. Performance from the fusion of ADS-B and MLAT improves an average of 51.51% when compared to the original data.

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.

Robust Filtering Algorithm for Improvement of Air Navigation System (항행시스템 성능향상을 위한 강인한 필터링 알고리즘)

  • Cho, Taehwan;Kim, Jinhyuk;Choi, Sangbang
    • Journal of Advanced Navigation Technology
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    • v.19 no.2
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    • pp.123-132
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    • 2015
  • Among various fields of the CNS/ATM, the surveillance field which includes ADS-B system, MLAT system, and WAM system is implemented. These next generation systems provide superior performance in tracking aircrafts. However, They still have error. In this paper, filtering algorithm is proposed in order to enhance aircraft tracking performance of ADS-B, MLAT, and WAM systems. The proposed method is a Robust Interacting Multiple Model filter, called Robust IMM filter, that improves IMM filter. The Robust IMM filter can not only improves the aircraft tracking performance but also track aircraft continually using estimates calculated from the filter when data losses occur. The simulation results of the proposed aircraft tracking methods show that the filtering data provides a better performance up to an average of 19.21%.

Performance Analysis of MLAT System Receiver for Aircraft Flight Control System

  • Yoo, Sang-Hoon;Oh, Jeong-Hun;Koh, Young-Mok;Kim, Su-Hong;Sung, Tae-Kyung
    • Journal of Positioning, Navigation, and Timing
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    • v.5 no.1
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    • pp.29-36
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    • 2016
  • In this paper, performance on receivers of multilateration (MLAT) system that uses ADS-B signal, which is recently becoming popular, was analyzed to overcome shortcomings of existing aircraft flight control systems or reinforce the capabilities. A link budget was analyzed using a channel model in the airport environment with regard to Local Area Multilateration (LAM) for ground-controlled landing around the airport. In order to detect signals that arrived at the receiver successfully, sensitivity of receiver was analyzed using a signal-to-noise ratio (SNR) worksheet, and a method that improves accuracy of the distance measurement was proposed by adopting a peak estimation using sampling signals. Through simulations, optimum specifications of receivers were analyzed to have high precision positioning of LAM, and accuracy of LAM distance measurements was presented.

Air Surveillance Using Mode-S Multilateration (모드-S 다변측정법을 이용한 항공감시기술 분석 및 전망)

  • Kim, Chang-Hwan;Han, Jae-Hyun;Kang, Ja-Young
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.18 no.3
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    • pp.9-20
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    • 2010
  • Surveillance is an enabler of safety with respect to aircraft separation and as a consequence capacity and efficiency with respect to aircraft operations. The new emerging technology among modern civil aviation surveillance is Multilateration (MLAT) which would affect on the surveillance capacity with both side of surveillance signal and operational properties. Multilateration system is needed to receive the signal which must reach at least 3 ground receivers simultaneously and has the effect that will have on with the ultimate accuracy. In this paper, the principle and the system configuration are reviewed. And its benefit of development is considered with use in situations where it is difficult to locate tranditional radar. This MLAT requires no additional avionics equipment to supply service with more accurate and less expensive. And it is able to enhance performance that meets international standards and extend the investment of air navigation service providers with reducing environmental impact by utilizing a small footprint on existing structures. Finally, it can be added to meet a wide range of coverage requirements and future surveillance needs.

Performance Analysis of Pulse Positioning Using Adaptive Threshold Detector (ATD)

  • Chang, Jae Won;Lee, Sang Jeong
    • Journal of Positioning, Navigation, and Timing
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    • v.7 no.1
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    • pp.25-35
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    • 2018
  • This paper describes the measurement of pulse positioning (input time) to calculate a time of arrival (TOA) that takes from transmitting a signal from the target of multilateration (MLAT) system to receiving the signal at the receiver. In this regard, this paper analyzes performances of simple threshold method and level adjust system (LAS) method, which is one of the adaptive threshold detector (ATD) methods, among many methods to calculate pulse positioning of signal received at the receiver. To this end, Cramer-rao lower bound (CRLB) with regard to pulse positioning, which was measured when signals transmitted from a transponder mounted at the target were received at the receiver, was induced and then deviation sizes with regard to pulse positioning, which was measured with simple threshold and LAS methods through MATLAB simulations, were compared. Next, problems occurring according to a difference in amplitude of signals inputted to each receiver are described when pulse positioning is measured at multiple receivers located at a different distance from the target as is the case in the MLAT system. Furthermore, LAS method to resolve the problems is explained. Lastly, this study analyzes whether a pulse positioning error occurring due to the signal noise satisfies the requirement (6 nsec. or lower) recommended for the MLAT system when using these two methods.