• Title/Summary/Keyword: Line-of-sight Analysis

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Performance Analysis of Real-Time Video Management System Based on Multi-Hop Wi-Fi Direct Communication (멀티 홉 Wi-Fi Direct 통신 기반 실시간 영상관리 시스템 성능 분석)

  • Woo, Chae-yul;Jo, Mi-ran;Kwon, Soon-ryang
    • The Journal of Korean Institute of Communications and Information Sciences
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    • v.41 no.11
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    • pp.1472-1480
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    • 2016
  • When disasters such as earthquake, flood, typhoon, fire and terrorism are occurred a video management system is required which can shoot video on the disaster site, and send it to a server located in the command center that can grasp at a glance the site conditions. In this paper, to know the performance elements information needed to construct the video management system. we presented a method of configuring an ad hoc network based on Wi-Fi direct communication. And we also evaluated the performance through built of environment for the video management system. The evaluated performance test items are 'packet flow tests according to the video compression ratios and the image sizes', 'packet flow tests according to the distance and traffic tests', 'packet flow tests according to whether LOS or not', and 'performance test of scenarios'.

Prediction of Strength and Propagation Characteristics of Supersonic Flight Sonic Boom (초음속 비행체의 소닉붐 강도와 전파 특성 예측)

  • Jung, Suk Young;Ha, Jae-hyoun;Lee, Younghwan;Jin, Hyeon
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.48 no.7
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    • pp.497-504
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    • 2020
  • A technique was developed for analysis on sonic boom created by supersonic flight and for prediction of its sound level and atmospheric propagation characteristics. It is of great importance to anticipate sound level of sonic boom because it causes environmental issue. For that purpose, the simplified sonic-boom prediction method was applied to calculate sound pressure according to physical properties and flight information of the object and distance to measurement site, in this study. Propagation characteristics of shock wave emanated from a flying object was analyzed by using line-of-sight vector and ray tracing method which dealt with refraction of wave due to atmospheric density distribution along altitude. Predicted results agreed well with measured data from real flight.

Effective Decision of the Route Alignment with Digital Terrain (수치지형모형을 이용한 효율적인 노선결정)

  • Kang, Joon-Mook;Yoon, Hee-Cheon;Lee, Hyung-Seok;Lee, Sung-Soong
    • Journal of Korean Society for Geospatial Information Science
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    • v.4 no.2 s.8
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    • pp.195-203
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    • 1996
  • The 3-D analysis of terrain for route design and selection is being used as important basic data for effective judgement of political draft. This study is to decide efficient alignment of the entry route and design bridge by modeling, analyzing and displaying surface with digital terrain data. In this study we analyze slope, aspect, shaded-relief, line of sight and watershed on the base of DTM such as contour, TIN and grid. And we can not only esti mate end-area volume for road construction by calculating cut and fill and displaying mass-curve but also recognize the scene after execution with simulation of road and terrain. The result of this study reveals that visual effects of the 3-D terrain data are very effective for designer and decisionmaker to select and review alternative route with regard to terrain characteristics.

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Homing Loop Design for Missiles with Strapdown Seeker (스트랩다운 탐색기 기반 호밍루프 설계)

  • Hong, Ju-Hyeon;Ryoo, Chang-Kyung
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.42 no.4
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    • pp.317-325
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    • 2014
  • For a missile with a strapdown seeker, line-of-sight rate for guidance is obtained by compensating the look angle rate from the strapdown seeker by the body angular rate from rate gyros. However, the body angular rate from rate gyros has different signal properties when it compared to the body angular rate implicitly included in the look angle rate. Typically this discrepancy causes instability of homing loop. In this paper, we propose a design method of homing loop where seeker delay is compulsively placed in the output signal of the rate gyros for accordance of both body rates. Also, PID control loop is considered for obtaining stabilized guidance command even though uncertainties of seeker delay is associated. The stability analysis for the linear homing loop before and after the compensation has been done. The stability and performance of the designed terminal homing loop is verified through full nonlinear 6-DOF simulations.

A Voice Coding Technique for Application to the IEEE 802.15.4 Standard (IEEE 802.15.4 표준에 적용을 위한 음성부호화 기술)

  • Chen, Zhenxing;Kang, Seog-Geun
    • Journal of Broadcast Engineering
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    • v.13 no.5
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    • pp.612-621
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    • 2008
  • Due to the various constraints such as feasible size of data payload and low transmission power, no technical specifications on the voice communication are included in the Zigbee standard. In this paper, a voice coding technique for application to the IEEE 802.15.4 standard, which is the basis of Zigbee communication, is presented. Here, both high compression and good waveform recovery are essential. To meet those requirements, a multi-stage discrete wavelet transform (DWT) block and a binary coding block consisting of two different pulse-code modulations are exploited. Theoretical analysis and simulation results in an indoor wireless channel show that the voice coder with 2-stage DWT is most appropriate from the viewpoint of compression and waveform recovery. When the line-of-sight component is dominant, the voice coding scheme has good recovery capability even in the moderate signal-to-noise power ratios. Hence, it is considered that the presented scheme will be a technical reference for the future recommendation of voice communication exploiting Zigbee.

Study on Data-link Antenna System for UAV (무인기용 탑재 데이터링크 안테나 시스템에 관한 연구)

  • Yeo, Su-Cheol;Kang, Byoung-Wook;Bae, Ki-Hyeong;Yoon, Chang-Bae
    • The Journal of the Korea institute of electronic communication sciences
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    • v.15 no.1
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    • pp.9-14
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    • 2020
  • In this paper, we studied on-board antenna(primary link/secondary link/satellite link) used in UAV Data-link system. As a result, it is ideal to configure the Data-link as a triple link to secure the flight stability of the UAV, but the communication link should be configured according to the operating platform. As a result of overseas R&D trend analysis, the on-board Data-link antenna is installed and operated in a location where it is easy to secure LOS. The primary link consists of a directional antenna for basic operation and an omni-directional antenna for emergency operation. The secondary link uses a monopole/dipole antenna in the UHF/C band. Satellite link has been developed to apply phased array antenna to improve UAV operability.

A Study on Basic Modeling Method for MTF Analysis of Observation Satellites (관측위성의 MTF 해석을 위한 기본 모델링 기법 연구)

  • Kim, Do-Myung;Kim, Deok-Ryeol;Kim, Nak-Wan;Suk, Jin-Young;Kim, Hee-Seob;Kim, Gyu-Sun;Hyun, Young-Mok
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.36 no.5
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    • pp.472-482
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    • 2008
  • A modulation transfer function(MTF) tree is established to estimate the overall MTF of an observation satellite and to analyze the image performance. Basic MTF models relevant to each MTF tree component are represented as mathematical relationship between optics-structural dynamics, thermal deformation, attitude and dynamic characteristics of a satellite and the effects due to the space environment. The Basic MTF models consist of diffraction limited MTF with central obscuration, aberration, defocus, line-of-sight(LOS) jitter, linear motion, detector integration, and so forth. Performance estimation is demonstrated for a virtual earth-observation satellite in order to validate the constructed modeling method. The proposed models enable the system engineers to calculate the overall system MTF and to determine the crucial design parameters that affect the image performance in the conceptual design phase of an observation satellite.

Performance Analysis of Low Earth Orbit Satellite Communication Systems Under Multi-path Fading Environments (다중경로 페이딩 환경하에서의 저궤도 위성통신시스템 성능 분석)

  • Hae-uk Lee;Young-bin Ryu;Hyuk-jun Oh
    • Journal of Advanced Navigation Technology
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    • v.27 no.4
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    • pp.410-416
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    • 2023
  • Unlike geostationary satellite communication systems, low-earth orbit(LEO) satellite communication systems move at relatively high speeds, and the angle with the ground device is not fixed and varies over a wide range. The propagation channel condition between satellites and ground nodes cannot be assumed line of sight(LOS) anymore. This paper analyzes the low-orbit multi-path fading satellite channel model that can occur in LEO satellite communication systems and Doppler frequency transition caused by high-speed maneuvering of LEO satellites and presents effective equalization techniques for OFDM and SC-FDE transmission methods suitable for multi-path frequency selective fading satellite channel models. In addition, this paper compares and analyzes the performance of OFDM and SC-FDE transmission methods in multipath fading LEO satellite channel environment using the proposed equalization techniques through simulations. Simulation results showed that SC-FDE outpeformed OFDM.

Aeronautical Link Availability Analysis for the Multi-Platform Image & Intelligence Common Data Link (다중 플랫폼 영상정보용 공용 데이터링크의 링크 가용도 성능 분석)

  • Ryu, Young-Jae;Ryu, Jung-Hun;Pak, Ui-Young
    • The Journal of Korean Institute of Communications and Information Sciences
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    • v.37C no.10
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    • pp.965-976
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    • 2012
  • Multi-Platform Image and Intelligence Common data link(MPI-CDL) systems are designed to transmit the imaginary and signal intelligence data at an aeronautical to ground line of sight(LOS) link. This paper proposes a method to predict a link availability and analyzes the required link margin to satisfy a given link availability for MPI-CDL systems. To estimate a link availability the proposed method applies the conditional probability so that both a rain attenuation and a multipath fading are considered simultaneously. Link margins to meet the link availability for MPI-CDL systems are calculated according to an operating environment including frequencies, flight altitudes and transmission ranges. The required link margins for actual unmanned air vehicle systems are also given by simulation results.

RF Seeker LOS Rate Estimation Method using Covariance and Signal Management (공분산 및 신호관리를 이용한 RF탐색기 시선각 변화율 추정기법)

  • Moon, Gwan-Young;Jun, Byung-Eul
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.40 no.4
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    • pp.292-299
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    • 2012
  • The line-of-sight(LOS) rate is estimated using Kalman filter in Radio-Frequency(RF) seeker. For the two axis gimbaled seeker, proper system modeling is considered and the basic filter structure is set up. The main issue for Kalman filter is choosing the proper process and measurement noise. For the measurement process, the signal to noise ratio(SNR) and other components are introduced. To cope with the eclipse problem or other abnormal seeker status, the pseudo input signal concept is proposed. By conditioning abnormal signals, the LOS rate estimation performance is increased. The process noise is also an important factor in the propagation phase. The analytical approach on a process noise component is performed and a reliable region for the filter is calculated based on the eigenvalue analysis. Some numerical simulations are performed to check the validity of suggested algorithm.