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๏ਓ ใ௨৴ձ THE INSTITUTE OF ELECTRONICS, INFORMATION AND COMMUNICATION ENGINEERS ৴ใ IEICE Technical Report ՐඈߦػͷϚΠΫϩແઢڅڙ༻ૹγεςϜʹΔ ݕͷ ڀݚؠਗ਼ਫ ༏ 1 ୩ ༑ 1 ݪ ؽ1 ʑ 2 ฏԬ ژ2 ߐ2 ถຊ ߒҰ 2 1 ژେ ੜଘڀݚݍ˟ 611–0011 ژӉޒࢢϲঙ 2 ۀେେӃ E-mail: 1{masashi iwashimizu,mitani,shino}@rish.kyoto-u.ac.jp 2{[email protected]} Β· ՐඈߦػͷԽΛਤΔΊɺΤωϧΪʔΛϚΠΫϩʹΑແઢڅڙΔɻຊڀݚͰඈ ػߦͷݕγεςϜΛڀݚɻඈػߦΒ৴ΕΔύΠϩοτ৴߸ΛͷΞϨΠΞϯςφͰड৴ɺΕΒͷ ड৴Ґ૬Λ༻ݕΛߦɻҐ૬ݕग़ʹݕΛ༻ɻԽͷΊඈʹػߦΔϨΫς φʹੜΔୈ 2 ߴௐΛύΠϩοτ৴߸ͱ༻ΔɻඈʹػߦૹΛߦɺੜΔୈ 2 ߴΛ༻ݕݧΛߦɻݧͰ΄΅શͷʹݕՄͰɺड৴Ͱ ޡେͳɻͷݪҼෳͷϨΫςφߴௐΛੜɺϑΣʔζυΞϨʔͱৼΔΒͰ Δͱɻ Ωʔϫʔυ Րඈߦػ, ݕ, ౸དྷਪఆ, 2 ߴStudy on Direction Detection in a Microwave Power Transmission System for a Mars Observation Airplane Masashi IWASHIMIZU 1 , Tomohiko MITANI 1 , Naoki SHINOHARA 1 , Gaku SASAKI 2 , Kei HIRAOKA 2 , Koyo MATSUZAKI 2 , and Koichi YONEMOTO 2 1 Research Institute for Sustainable Humanosphere, Kyoto University Gokasho, Uji, Kyoto, 611–0011 2 Graduate school of Engineering, Kyushu Institute of Technology E-mail: 1{masashi iwashimizu,mitani,shino}@rish.kyoto-u.ac.jp 2{[email protected]} Abstract In order to attain the weight saving of a Mars observation airplane, we are planning to supply energy by microwave. This paper presents the direction detection of the airplane. An array antenna on the ground receives a pilot signal from the airplane, and detects the direction of the airplane by phase dierences of antenna elements. For weight saving, we utilize the second harmonics radiated from rectennas on the airplane as a pilot signal. Key words Mars Observation Airplane, Direction Detection, Direction of Arrival Estimation, Second Harmonics 1. ࡏݱՐͰܕߦͷ୳ػ׆༂Δɻ୳ ػΛߦΔ߹ɺՐද໘ͷʹ·ΕҠಈ ɻͰඈߦʹػΑΔՐ୳ఏҊΕΔɻ Րͷେؾʹٿ0.75 ˋͱඇৗʹখ Ί༲ΛडʹɻຊڀݚͰόοςϦʔΛখ ܕԽػମͷԽΛਤΔΊʹਤ 1 ʹΑʹՐΒ୳ ػແઢڅڙΛߦͱΛఏҊΔɻ୳ʹػϨΫς φΛෑ٧ΊΔͱͰͷڅڙΛडΔɻҎલɺຊڀݚͰ 2 ʹΑʹখܕػߦͷૹΛखಈͰඌΔݧΛ ߦɻݧͰ 15 ݸͷϨΫςφΛػߦΛઢඈ ߦΔͱʹɻຊڀݚͰඈػߦΛಈͰඌΔ ͱΛతͱɺඈػߦͷݕͷڀݚΛߦɻ

Study on Direction Detection in a Microwave Power Transmission …wpt/paper/WPT2013-37.pdf · 2017. 1. 17. · Study on Direction Detection in a Microwave Power Transmission System

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  • THE INSTITUTE OF ELECTRONICS,INFORMATION AND COMMUNICATION ENGINEERS

    IEICE Technical Report

    1 1 1 2 2

    2 2

    1 611–0011

    2

    E-mail: 1{masashi iwashimizu,mitani,shino}@rish.kyoto-u.ac.jp2{[email protected]}

    2 2

    , , , 2

    Study on Direction Detection in a Microwave Power Transmission System

    for a Mars Observation Airplane

    Masashi IWASHIMIZU1, Tomohiko MITANI1, Naoki SHINOHARA1, Gaku SASAKI2, Kei

    HIRAOKA2, Koyo MATSUZAKI2, and Koichi YONEMOTO2

    1 Research Institute for Sustainable Humanosphere, Kyoto University Gokasho, Uji, Kyoto, 611–0011

    2 Graduate school of Engineering, Kyushu Institute of Technology

    E-mail: 1{masashi iwashimizu,mitani,shino}@rish.kyoto-u.ac.jp2{[email protected]}

    Abstract In order to attain the weight saving of a Mars observation airplane, we are planning to supply energy

    by microwave. This paper presents the direction detection of the airplane. An array antenna on the ground receives

    a pilot signal from the airplane, and detects the direction of the airplane by phase differences of antenna elements.

    For weight saving, we utilize the second harmonics radiated from rectennas on the airplane as a pilot signal.

    Key words Mars Observation Airplane, Direction Detection, Direction of Arrival Estimation, Second Harmonics

    1.

    0.75

    1

    2

    15

    mitan_000WPT2013-37(2014-03)

    mitan_000This article is a technical report without peer review, and its polished and/or extended version may be published elsewhere.

  • THE INSTITUTE OF ELECTRONICS,INFORMATION AND COMMUNICATION ENGINEERS

    IEICE Technical Report

    2.

    2. 1

    2.445GHz 900W

    +15.5 dBi

    3

    11 deg.

    2. 2

    1 [1]

    2

    3

    4

    (i)

    (ii) δ (i) (iii)

    ζ θ ϕ (1) (2)

    θ = sin−1

    ⎝ δ

    π

    √1−

    (ζπ

    )2

    ⎠ (1)

    ϕ = sin−1(ζπ

    )(2)

    |δ|

  • THE INSTITUTE OF ELECTRONICS,INFORMATION AND COMMUNICATION ENGINEERS

    IEICE Technical Report

    2. 4 2

    2

    4.89GHz

    2 6 7

    3m

    1.5m

    2.445GHz 900W

    x-y -30 deg.

    30 deg.

    4.89GHz

    8

    -35 dBm -60 dBm 2

    2

    3.

    3. 1

    2.445GHz 900W 4.89GHz

    6 2

    7 2

    6

    4.89GHz -75 dBm

    4.89GHz

    -30 dBm -70 dBm x-y

    -30 deg.

    30 deg.

    9

    -60 dBm

    -60 dBm

    3. 2

    8 2

    9

  • THE INSTITUTE OF ELECTRONICS,INFORMATION AND COMMUNICATION ENGINEERS

    IEICE Technical Report

    6 7

    AGC AGC

    10

    AGC

    3. 3

    11 1

    θ1 θ2

    3m

    λ/2

    θ1 θ2

    δ (3)

    δ = πsinθ1 (3)

    12 2

    λ 1 0.9

    13 13

    f(θ) δ (4)

    δ = f(θ2)− f(θ1) + πsinθ1 (4)

    13

    f(θ2)−f(θ1)θ1 30 deg. θ2 30.4 deg. f(θ2)−f(θ1)

    18.7 deg. 7.1 deg.

    2

    15

    f(θ)

    10

    10 AGC

    4.

    [1] A. Nagahama, T. Mitani, N. Shinohara, K. Fukuda, K. Hi-

    raoka, and K. Yonemoto “Auto Tracking and Power Con-

    trol Experiments of a Magnetron-based Phased Array Power

    Transmitting System for a Mars Observation Airplane”,

    IEEE MTT-S IMWS-IWPT 2012, Kyoto, Japan, May 10-

    11.

    11

    12

    13