• Title/Summary/Keyword: S-Band Antenna Selection

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Test-bed Design for the Evaluation of Wireless Communication System on Small Launch Vehicle (소형 발사체 무선 통신시스템 검증을 위한 테스트 베드 설계)

  • Lee, Dae-Hyun;Oh, TaeckKeun;Park, Dong-Hwa;Lee, Hong-Ki;Park, Dong-Hyun;Song, Ho-Jin
    • Journal of Advanced Navigation Technology
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    • v.22 no.4
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    • pp.311-318
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    • 2018
  • In this paper, test-bed for the evaluation of wireless communication system on a small launch vehicle is proposed. The proposed test-bed consists of antenna test-coupler, RF attenuators, and RF switch modules. The antenna test-coupler isolates antennas for each band and transmits / receives wireless signals. The RF attenuator and switch are used for path selection of testing signal path. In design and measurement result of the antenna test-coupler, the antenna test-coupler has shielding effect higher than 39.3, 47.1, 56.1 dB at UHF-, S-, X-band. Through testing on small launch vehicle wireless communication system, we were able to successfully transmit and receive data between each test system and launch vehicle with antenna path switching.

Dual-Band Frequency Reconfigurable Small Eighth-Mode Substrate-Integrated Waveguide Antenna (이중 대역 주파수 가변 1/8차 소형 기판집적형 도파관 안테나)

  • Kang, Hyunseong;Lim, Sungjoon
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
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    • v.25 no.1
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    • pp.10-18
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    • 2014
  • In this paper, we propose a new frequency reconfigurable dual-band antenna. By using an electronically compact eighth-mode substrate-integrated-waveguide(EMSIW) resonator, we have designed a compact antenna, which performs dual-band movement by additionally loading a complementary split ring resonator(CSRR) structure. The EMSIW and CSRR structures are designed to satisfy the bandwidths of 1.575 GHz(GPS) and 2.4 GHz(WLAN), respectively. We load the CSRR with a varactor diode to allow a narrow bandwidth and to enable the resonance frequency to continuously vary from 2.4 GHz to 2.5 GHz. Thus, we realize a channel selection function that is used in the WLAN standards. Irrespective of how a varactor diode moves, the EMSIW independently resonates so that the antenna maintains a fixed frequency of the GPS bandwidth even at different voltages. Consequently, as the DC bias voltage changes from 11.4 V to 30 V, the resonance frequency of the WLAN bandwidth continuously changes between 2.38 GHz and 2.5 GHz, when the DC bias voltage changes from 11.4 V to 30 V. We observe that the simulated and the measured S-parameter values and radiation patterns are in good agreement with each other.

Inter-Cell Cooperative Scheduling with Carrier Aggregation in LTE-Advanced System (LTE-Advanced 시스템의 반송파 집성(Carrier Aggregation)을 고려한 셀간 협력 스케쥴링 기법)

  • Yang, Chan S.;Cho, Kumin;Yu, Takki;Kang, Chung G.
    • The Journal of Korean Institute of Communications and Information Sciences
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    • v.39B no.3
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    • pp.151-161
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    • 2014
  • 3GPP LTE-Advanced (Release 10) system specifies carrier aggregation (CA) to enable high data rate on using multiple frequency bands, including the variout CA-specific deployment scenarios. Considering one of those scenarios in which the different directional sector antenna is employed by each frequency band, we propose a per-carrier cell selection scheme that can improve the average throughput of the cell-edge users by allowing each user equipment (UE) to select the frequency band of the adjacent cell. Furthermore, a distributed algorithm for inter-cell copperative scheduling in this scheme is proposed to support proportional fairness among the cells. It has been shown that the proposed scheduling algorithm for the per-carrier cell selection scheme improves the cell-edge user throughput roughly by 50% over that of the conventional scheme.

Papers : Attitude Determination Algorithm of LEO Satellites in the Sun - Acquisition Mode (논문 : 태양획득 모드에서 저궤도 위성의 자세결정 알고리즘)

  • An,Hyo-Seong;Lee,Seon-Ho;Lee,Seung-U;Chae,Jang-Su
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.30 no.1
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    • pp.82-87
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    • 2002
  • The attitude determination in LEO Satellite like KOMPSAT is one of the most important issues for Sun-Acquisition. Particularly, in KOMPSAT, the roll axis direction can be determined since the sun sensor gives the information on the Euler angle for pitch and yaw axes in Sun-Acquisition mode. In other words, it is the problem to determine the two unknown axes direction with one axis knowledge. This paper proposes a new effective method for attitude determination of general LEO satellites when one axis information is avilable and proves its usefulness throughout the simulation.