• Title/Summary/Keyword: Aeronautical communications

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Roll/Yaw Momentum Management Method of Pitch Momentum Biased Spacecraft (피치 모멘텀 바이어스 위성시스템의 롤/요축 모멘텀 제어방식)

  • Rhee, Seung-Wu;Ko, Hyun-Chul;Jang, Woo-Young;Son, Jun-Won
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.37 no.7
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    • pp.669-677
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    • 2009
  • In general, the pitch momentum biased system that induces inherently nutational motion in roll/yaw plane, has been adapted for geosynchronous communications satellites. This paper discusses the method of roll attitude control using yaw axis momentum management method for a low earth orbit(LEO) satellite which is a pitch momentum biased system equipped with only two reaction wheels. The robustness of wheel momentum management method with PI-controller is investigated comparing with wheel torque control method. The transfer function of roll/yaw axis momentum management system that is useful for attitude controller design is derived. The disturbance effect of roll/yaw axis momentum management system for attitude control is investigated to identify design parameters such as magnitude of momentum bias and to get the insight for controller design. As an example, the PID controller design result of momentum management system for roll/yaw axis control is provided and the simulation results are presented to provide further physical insight into the momentum management system.

Development of System Performance Analysis Simulator for Spaceborne Synthetic Aperture Radar (위성용 영상레이더 시스템 성능 분석 시뮬레이터 개발)

  • Won, Young-Jin;Lee, Jae-Hyun
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.45 no.4
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    • pp.318-327
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    • 2017
  • Synthetic Aperture Radars (SARs) that can be performed regardless of weather and day-and-night conditions have been developed for Earth remote sensing in recent decades. Korea Aerospace Research Institute (KARI) has developed and launched successfully the KOrea Multi-Purpose SATellit-5 (KOMPSAT-5) which is the first Korean SAR satellite in 2013, and is currently developing the KOMPSAT-6 which is the next generation series of the SAR satellite. This paper describes the development of the system performance analysis simulator which is necessary for spaceborne SAR payload design and analysis. The system performance analysis simulator consists of the antenna pattern generation simulator, the SAR performance analysis simulator, and the image quality analysis simulator. The simulation results of this research show that this simulator can be applicable as the design and analysis tool for the spaceborne SAR payload system during the design phase.

Conceptual Design of KASS Uplink Station (한국형 위성항법보강시스템(KASS) 위성통신국 기본 설계)

  • You, Moonhee;Sin, Cheon Sig
    • Journal of Satellite, Information and Communications
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    • v.12 no.4
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    • pp.72-77
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    • 2017
  • The Satellite Based Augmentation System (SBAS) broadcasts to users integrity and correction information for Global Navigation Satellite System (GNSS) such as GPS and GLONASS using geostationary orbit (GEO) satellites. In accordance with the recommendation of the International Civilian Aeronautical Organization (ICAO) to introduce SBAS until 2025, a Korean SBAS system development / construction project is underway with the Ministry of Land, Transport and Maritime Affairs. Korea Augmentation Satellite System (KASS) is a high precision GPS correction system which is composed of KASS Reference Station (KRS), KASS Processing Station (KPS), KASS Uplink Station (KUS), KASS Control Station (KCS) and GEO satellites. In this paper, we provided the conceptual design of the KASS uplink station, which is composed of the Signal Generator Section (SGS) and the Radio-Frequency Section (RFS), and interface between the KASS ground sector and the GEO satellite.

Modeling & Performance Analysis of the MAC Protocol for VDL in the Aeronautical Mobile Communication System (항공이동통신 시스템에서 VDL을 위한 MAC 프로토콜 모델링 및 성능 분석)

  • Kim, Yong-Joong;Park, Hyo-Dal
    • Journal of Advanced Navigation Technology
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    • v.13 no.3
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    • pp.327-336
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    • 2009
  • This paper analysis the STDMA protocol in aviation wireless data communications and carry out the performance analysis with simulation. The STDMA protocol that is currently being used in VDL Mode-4 has TDMA system characteristics, which provides time-division into several slots per one frame. The results of modeled STDMA protocol's data channel analysis show approximate 0.7 channel throughput at the transmission probabilities 0.045, 0.2, and 0.3 in the aspects of channel throughput. The delay time are 2.32434sec, 2.0293sec, and 2.12128sec respectively. These results shows the good stability in spite of variable transmission probabilities. Consequently, it is expected that STDMA protocol would be used properly for domestic communication demands and supervision system improvement by means of applying this to point-to-point communication and data/location broadcasting as a fundamental technology in CNS/ATM.

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A Study on the Implementation Scenarios of GNSS Augmentation System for Korean Airspace (우리나라 전공역 위성항법 보강시스템 구현 방안 연구)

  • Bae, Joong-Won;Kim, Dong-Min;Jee, Gyu-In
    • Journal of Advanced Navigation Technology
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    • v.12 no.6
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    • pp.567-573
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    • 2008
  • According to the ICAO's Global Air Navigation Plan for CNS/ATM - Communications, Navigation, and Surveillance - systems, employing digital technologies, including satellite systems together with various levels of automation, are to be applied in support of a seamless global air traffic management system. For the future navigation, the focus of future implementation efforts can be placed entirely on an expected gradual migration toward GNSS-based navigation, Korea has been considered various options for airspace GNSS augmentation system: GBAS, SBAS and GRAS. This paper discusses current status and future trend of GNSS airspace navigation systems, and presents the results of possible augmentation options and scenarios to analyze system availabilities which could lead to the conclusion of the best program for Korea. The results showed that Korea could have sufficient availabilities from en-route to CAT-I approach with ABAS and GBAS. The study was in cooperated with MITRE, an American research company.

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Aeronautical to Ground Channel Modeling for Common Data Link (공용데이터링크를 위한 공대지 채널 모델링)

  • Park, Hongseok;Shim, Jae-Nam;Kim, Donghyun;Kim, Dong Ku
    • The Journal of Korean Institute of Communications and Information Sciences
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    • v.41 no.12
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    • pp.1876-1883
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    • 2016
  • The new channel model for high data rate common data link(CDL) is proposed. The Two-ray channel, which is composed of the reflected signals on the front ground of the receiver, is considered in this paper. This channel arises due to the curvature of the earth when the altitude of the transmitter is tens of kilometers and distance between the transmitter and the receiver is hundreds of kilometers. The Two-ray channel is modeled by estimating the maximum delay profile and the power delay profile, depending on the transmitting and receiving beamforming angle and the radiation pattern of antenna. The power delay profile has a larger effect on the bit error rate(BER) over signal to noise ratio(SNR) than the maximum delay profile, because the distance range is too long in the proposed channel model.

A Design Verification for the EQM CBS Ka-band Payload System by EMC Test (EQM 통신방송위성 KA대역 탑재체 시스템의 EMC 시험을 통한 검증)

  • Lee,Ho-Jae;U,Hyeong-Je;Sin,Dong-Hwan;Park,Jong-Heung
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.31 no.10
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    • pp.97-104
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    • 2003
  • This paper addresses EMC test results for the EQM Communications & Broadcasting Satellite(CBS) Ka-band Payload System. The aim of the EMC test is to verify that the payload system has no effect on the other system and is not affected by the external field. The compliance of EMC system requirements was verified by the analysis and measurement of the emission level from the payload system. The variation of performance by noise injection was measured to inspect the susceptibility of the payload system. The analysis and test results also showed that the electromagnetic interference has no serious effect on the overall payload system performance. It is confirmed that the EQM CBS Ka-band payload system can be operable in the space environment from the EMC performance's viewpoint. It is also obtained that better performance can be acquired by improving waveguide design and integration method.

Orbit Design of a Korean Regional Communication & Navigation Satellite System (한국형 지역 위성 통신항법시스템의 위성 궤도설계에 관한 연구)

  • Lee, Sang-Hyun;Park, Byung-Woon;Kim, Do-Yoon;Kee, Chang-Don;Paik, Bok-Soo;Lee, Ki-Hoon
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.33 no.7
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    • pp.51-58
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    • 2005
  • In 1990, GPS which had been developed for the military purposes became available to the civilian community. Since then these satellite navigation systems have been used extensively in the industrial areas such as car navigation, airplanes, communications, science and surveying. If we are dependent on GPS, however, there are some foreseeable problems in the areas of national security and sovereignty. Current GPS satellite constellation provides limited performance for the country like Korea and Japan where mountain area and urban canyon do not allow the wide skyline. To solve these problems, many countries plan to make other alternative navigation systems.In this paper, RNSS(Regional Navigation Satellite System) is designed to provide communication service with high elevation angle. It is shown, that system does not only have good navigation performance, but also improve GPS performance in Korea and its neighboring areas.

Improvement of Reception Noise During Formation Flight of Aircraft (항공기 편대 비행 중 수신 잡음 개선 연구)

  • Kwon, Jung-Hyuk;Seo, Hong-Eun;Lee, Wang-Sang
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.49 no.6
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    • pp.497-504
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    • 2021
  • This paper presents improvement of the reception noise suppression method during formation flights of aircraft. Since aircraft communication equipment is very important for flight mission and safety to perform the functions of internal/external communications, it is required to implement noise-free, clean communication quality, and transmitting/receiving functions. Therefore, the FTA (Fault Tree Analysis) analysis and failure search were performed on the reception noise, and the internal noise of the intercom that affected the reception noise and the none-transmition phenomenon was identified. We changed the multiple grounds of the intercom to a single ground and applied an improved method of filtering the DC Offset voltage. As a result, the voice quality of the communication system of the aircraft was improved through the reduction of the reception noise during formation flights, and it was verified by ground and flight tests.

Flight Path Measurement of Drones Using Microphone Array and Performance Improvement Method Using Unscented Kalman Filter (마이크로폰 어레이를 이용한 드론의 비행경로 측정과 무향칼만필터를 이용한 성능 개선법에 대한 연구)

  • Lee, Jiwon;Go, Yeong-Ju;Kim, Seungkeum;Choi, Jong-Soo
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.46 no.12
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    • pp.975-985
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    • 2018
  • The drones have been developed for military purposes and are now used in many fields such as logistics, communications, agriculture, disaster, defense and media. As the range of use of drones increases, cases of abuse of drones are increasing. It is necessary to develop anti-drone technology to detect the position of unwanted drones using the physical phenomena that occur when the drones fly. In this paper, we estimate the DOA(direction of arrival) of the drone by using the acoustic signal generated when the drone is flying. In addition, the dynamics model of the drones was applied to the unscented kalman filter to improve the microphone array detection performance and reduce the error of the position estimation. Through simulation, the drone detection performance was predicted and verified through experiments.