• Title/Summary/Keyword: Phased-array antenna

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Development of an Airborne Telemetry Relay System Using Aircraft (항공기를 이용한 텔레메트리 신호의 공중 중계시스템 개발)

  • Yeom, Hyeong-Seop;Oh, Jong-Hoon;Sung, Duck-Yong
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.40 no.1
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    • pp.93-100
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    • 2012
  • A telemetry signal occurs the line-of-sight problem by the effect of geography in flight test. A fixed relay system or a mobile relay system is used to solve that problem in general but we propose an airborne telemetry relay system using aircraft in this paper. An airborne telemetry relay system receives the telemetry signal of the test vehicle and then retransmits it to the ground system. The receiving antenna which is a phased array antenna can be tilted to ${\pm}30^{\circ}$ beam direction by beam-forming and track the rapidly moving test vehicle in effect. The relay pod which is mounted to an aircraft consists of the front antenna and the side antenna. It receives S-band signal and then down-converts the frequency to L-band signal. As a result, that can remove the frequency interference on an aircraft while retransmitting.

Nulling algorithm design using approximated gradient method (근사화된 Gradient 방법을 사용한 널링 알고리즘 설계)

  • Shin, Chang Eui;Choi, Seung Won
    • Journal of Korea Society of Digital Industry and Information Management
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    • v.9 no.1
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    • pp.95-102
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    • 2013
  • This paper covers nulling algorithm. In this algorithm, we assume that nulling points are already known. In general, nulling algorithm using matrix equation was utilized. But, this algorithm is pointed out that computational complexity is disadvantage. So, we choose gradient method to reduce the computational complexity. In order to further reduce the computational complexity, we propose approximate gradient method using characteristic of trigonometric functions. The proposed method has same performance compared with conventional method while having half the amount of computation when the number of antenna and nulling point are 20 and 1, respectively. In addition, we could virtually eliminate the trigonometric functions arithmetic. Trigonometric functions arithmetic cause a big problem in actual implementation like FPGA processor(Field Programmable gate array). By utilizing the above algorithm in a multi-cell environment, beamforming gain can be obtained and interference can be reduced at same time. By the above results, the algorithm can show excellent performance in the cell boundary.

5-Bit Digital Phase Shifter for 12 GHz Band Active Phased Array Antenna System (12 GHz대 능동 위상 배열 안테나 시스템을 위한 5-비트 디지털 위상 변위기)

  • 김경식;최익권
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
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    • v.13 no.3
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    • pp.308-315
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    • 2002
  • In this paper, the 5-bit digital phase shiftier with 10 InGaAs HEMTs is designed and fabricated for U.S. mobile DBS receiving active phased array antenna system in 12 GHz band. 11.25 $^{\circ}$, 22.5$^{\circ}$ and 45$^{\circ}$ phase bits are designed in leaded-line type. 90$^{\circ}$ and 180$^{\circ}$ phase bits are designed in reflection type combined with ring hybrid. The return loss more than 17.5 ㏈, insertion louts less than 7.8 ㏈, and maximum phase error of $\pm$6$^{\circ}$for 32 phase responses are measured in 12.2 GHz~ 12.7 GHz band.

X-Band 6-Bit Phase Shifter with Low RMS Phase and Amplitude Errors in 0.13-㎛ CMOS Technology

  • Han, Jang-Hoon;Kim, Jeong-Geun;Baek, Donghyun
    • JSTS:Journal of Semiconductor Technology and Science
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    • v.16 no.4
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    • pp.511-519
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    • 2016
  • This paper proposes a CMOS 6-bit phase shifter with low RMS phase and amplitude errors for an X-band phased array antenna. The phase shifter combines a switched-path topology for coarse phase states and a switch-filter topology for fine phase states. The coarse phase shifter is composed of phase shifting elements, single-pole double-throw (SPDT), and double-pole double-throw (DPDT) switches. The fine phase shifter uses a switched LC filter. The phase coverage is $354.35^{\circ}$ with an LSB of $5.625^{\circ}$. The RMS phase error is < $6^{\circ}$ and the RMS amplitude error is < 0.45 dB at 8-12 GHz. The measured insertion loss is < 15 dB, and the return losses for input and output are > 13 dB at 8-12 GHz. The input P1dB of the phase shifter achieves > 11 dBm at 8-12 GHz. The current consumption is zero with a 1.2-V supply voltage. The chip size is $1.46{\times}0.83mm^2$, including pads.

A Broadband Digital Step Attenuator with Low Phase Error and Low Insertion Loss in 0.18-${\mu}m$ SOI CMOS Technology

  • Cho, Moon-Kyu;Kim, Jeong-Geun;Baek, Donghyun
    • ETRI Journal
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    • v.35 no.4
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    • pp.638-643
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    • 2013
  • This paper presents a 5-bit digital step attenuator (DSA) using a commercial 0.18-${\mu}m$ silicon-on-insulator (SOI) process for the wideband phased array antenna. Both low insertion loss and low root mean square (RMS) phase error and amplitude error are achieved employing two attenuation topologies of the switched path attenuator and the switched T-type attenuator. The attenuation coverage of 31 dB with a least significant bit of 1 dB is achieved at DC to 20 GHz. The RMS phase error and amplitude error are less than $2.5^{\circ}$ and less than 0.5 dB, respectively. The measured insertion loss of the reference state is less than 5.5 dB at 10 GHz. The input return loss and output return loss are each less than 12 dB at DC to 20 GHz. The current consumption is nearly zero with a voltage supply of 1.8 V. The chip size is $0.93mm{\times}0.68mm$, including pads. To the best of the authors' knowledge, this is the first demonstration of a low phase error DC-to-20-GHz SOI DSA.

Power Beaming and Its Application to Aerospace Propulsion

  • Komurasaki, Kimiya
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2008.03a
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    • pp.881-885
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    • 2008
  • Wireless energy transmission system to a Micro Aerial Vehicle is now under development. A 5.8 GHz microwave phased array antenna and rectenna array receiver have been developed. An electric motor on a circling MAV model was driven by the transmitted power. In addition, 140GHz millimeter-waves of up to 1MW was beamed to a "Microwave Rocket" and its thrusting has been successfully demonstrated.

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Mechanical Alignment of Hull Mounted Phased Array Radar on the Separated Mast (분리된 마스트에 설치되는 선체고정 위상 배열 레이더의 기계적 정렬)

  • Seo, Hyeong-Pil;Kim, Dae-Han;Kim, Joon-Woo;Lee, Kyung-Jin;Cho, Kyu-Lyong
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.20 no.9
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    • pp.465-473
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    • 2019
  • This paper is meaningful as the first case where a 4 - sided hull-fixed phased array radar was installed on a mast separated from Korea and the alignment was verified. The mechanical alignment method was studied for accurately mounting two separate masts for naval ships and the 3D scanner for alignment. Hull-fixed phased array radar uses very high frequency, so the short wavelength can cause a phase difference of the device due to the small positional error. Since the array antenna is fixed with the hull, it has higher accuracy control than the rotary radar for 4 array surfaces. The study describes a method of checking the flatness of two radar masts manufactured at a factory, a method of aligning masts in a shipyard, and a method of aligning four array pad mounting surfaces. As a tool for this, a 3D laser scanner and a software-based method for comparing survey results with 3D CAD are used. This paper is meaningful as the first example of installing a four-sided hull-fixed phased array radar on a separate mast from a Korean naval ship and deriving a mechanical alignment method.

A Theoretical Design of RADANT Lens (RADANT 렌즈의 이론적 설계에 관한 연구)

  • Lee, Kee-Oh;Park, Dong-Chul
    • Journal of the Korea Institute of Military Science and Technology
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    • v.12 no.3
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    • pp.360-367
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    • 2009
  • In this paper, the RADANT phase scanning scheme and the transmission-type loaded line phase shifter scheme, which are applicable to the phased array systems, are studied. Using these two schemes, a theoretical method to design an electronic beam steering RADANT lens is introduced. The validity of the presented theoretical method is verified through the simplified circuit simulation results.

3-bit Optical True Time Delay for 10 GHz Phased Array Antennas Composed of Optical 2$\times$2 MEMS Switches and Fiber Delay Lines (2$\times$2 MEMS 스위치와 광섬유지연선로를 이용한 10 GHz 위상배열 안테나용 3-bit 광학적 실시간 지연선로)

  • 이백송;신종덕;김부균
    • Proceedings of the Optical Society of Korea Conference
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    • 2003.02a
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    • pp.320-321
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    • 2003
  • 위성통신 및 무선통신에서 안테나의 수신 감도를 향상시키기 위한 노력은 계속되어 왔다. 안테나의 지향성을 높이기 위하여 다수의 동형 단위 안테나들을 일정 방향으로 배열하여 안테나를 기계적으로 회전시키지 않고, 고정된 다수의 동형 단위 안테나들에서 방사되는 전파의 위상을 전자적으로 변화시켜 방사 빔을 주사하는 방법, 즉 위상배열 안테나(Phased Array Antenna)를 널리 사용하고 있다. 위상배열 안테나의 단위 안테나에서 방사되는 전파의 위상을 변화시키기 위해선 실시간 시간지연 시스템이 필요하다. (중략)

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Ka-band Compact AESA Antenna Unit Design for Seeker

  • Bongmo Kang;Ikjong Bae;Jaesub Han;Youngwan. Kim;Jaehyun Shin;Jihan Joo;Seonghyun Ryu
    • International Journal of Internet, Broadcasting and Communication
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    • v.16 no.1
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    • pp.330-338
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    • 2024
  • In this paper, a Ka-band high-output active phased array antenna device applicable to small radars and seekers was designed, and the improved performance was studied. The radiation device assembly consists of 1x8 arrangements, and the step flared notch antenna type. It shows low active reflection loss characteristics in broadband, and low loss characteristics by applying the air-strip feeding structure, and is designed to enable beam steering up to 45 degrees. The TRM(transmit receive module) output power is more than 2.0W per channel using GaN HPA in the transmitting path, and satisfies more than 25.0 dB gain and less than 6.0 dB noise figure in the receiving path. Accordingly, the Effective Isotropically Radiated Power(EIRP) of the antenna unit shows the performance of 0.00 dB or more and the receive gain-to-noise temperature ratio(G/T) of 0.00 dB/k or more. For demonstration, we have designed aforementioned planar array antenna which consists of 64 radiating elements having a size within 130 mm x 130 mm x 300 mm and weight of less than 4.9 kg..