HIGUCHI Takehiro

Affiliation

Faculty of Environment and Information Sciences, Division of Artificial Environment and Information

Job Title

Associate Professor

Date of Birth

1977

Research Fields, Keywords

Aerospace Engineering, Optimal Control, Non-linear Control

Mail Address

E-mail address

Related SDGs




The Best Research Achievement in Research Career 【 display / non-display

The Best Research Achievement in the last 5 years 【 display / non-display

Education 【 display / non-display

  •  
    -
    2005

    Yokohama National University   Doctor Course   Completed

  •  
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    2002

    Yokohama National University   Master Course   Completed

  •  
    -
    2000

    Yokohama National University   Graduated

Degree 【 display / non-display

  • Doctor of Engineering - Yokohama National University

  • Master of Engineering - Yokohama National University

Campus Career 【 display / non-display

  • 2014.10
     
     

    Duty   Yokohama National UniversityFaculty of Environment and Information Sciences   Division of Artificial Environment and Information   Associate Professor  

  • 2012.4
    -
    2014.9

    Duty   Yokohama National UniversityFaculty of Environment and Information Sciences   Division of Artificial Environment and Information   Assistant Professor  

  • 2007.11
    -
    2012.3

    Duty   Yokohama National UniversityInterdisciplinary Research Center   Specially Appointed Assistant Professor  

  • 2021.4
     
     

    Concurrently   Yokohama National UniversityInterfaculty Graduate School of Innovative and Practical Studies   Associate Professor  

  • 2018.4
     
     

    Concurrently   Yokohama National UniversityGraduate school of Engineering Science   Department of Mechanical Engineering, Materials Science and Ocean Engineering   Associate Professor  

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External Career 【 display / non-display

  • 2015.4
    -
    2017.3

     

  • 2005.4
    -
    2007.10

    Yamaguchi University   Graduate School of Science and Engineering   Assistant Professor  

Academic Society Affiliations 【 display / non-display

  • 2000
     
     
     

    The Japan Society for Aeronautical and Space Science

  • 2002
     
     
     

    American Institute of Aeronautics and Astronautics

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    The Japan Society of Mechanical Engineers

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    The Society for Instrument and Control Engineers

Research Areas 【 display / non-display

  • Frontier Technology (Aerospace Engineering, Marine and Maritime Engineering) / Aerospace engineering

  • Informatics / Mechanics and mechatronics

Qualification acquired 【 display / non-display

  • Aviation Radio Operator

 

Research Career 【 display / non-display

  • Periodic Optiomal Controller for Multi-Joint Space structure

    Project Year:

  • Attitude Control of Satellites using CMGs

    Project Year:

  • Automatic Flight Control of Indoor UAVs

    The Other Research Programs  

    Project Year:

  • Automatic Flight Control of UAVs

    Grant-in-Aid for Scientific Research  

    Project Year:

  • Controller Design for Super Multi-Joint Space structure

    Project Year:

Books 【 display / non-display

  • Advances in the Astronautical Sciences:Applications of Space Technology for Humanity

    上野誠也( Role: Joint author)

    Univelt Inc. 

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    Language:English Book type:Scholarly book

  • Numerical Analysis Theory and Application

    J. Awrejcewicz, et. al.( Role: Joint author)

    InTech  ( ISBN:9789533073897

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    Language:English Book type:Scholarly book

  • Advances in the Astronautical Sciences:Space Activities and Cooperation Contributing to All Pacific Basin Countries

    上野誠也( Role: Joint author)

    Univelt Inc. 

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    Language:English Book type:Scholarly book

Papers 【 display / non-display

  • Semi-Optimal Control Using Shooting Method for Real Time Minimum-Time Maneuver of Satellite with VSCMG

    Tsuchiya Mitsuyoshi, Higuchi Takehiro

    AEROSPACE TECHNOLOGY JAPAN, THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES   20 ( 0 )   9 - 18   2021.4

    DOI CiNii

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    Language:Japanese   Publishing type:Research paper (scientific journal)   Publisher:THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES   Joint Work  

    <p>This study explores the minimum-time attitude maneuver of satellites using Control Moment Gyros (CMG). The CMG system is able to generate high torque and run for longer term than other actuators. However, it is known that the singular input that cannot generate effective torque appears in the optimal control for the minimum-time maneuver of a rigid spacecraft with a pyramid type SGCMG system. In previous studies, a new system equipped with variable speed CMG (VSCMG) to the CMG where the singular input appeared has been proposed. It is shown that the new system can rotate faster than the normal pyramid type SGCMG system in the simulation based on the optimal control law. However, for applications in actual satellites, numerical optimization cannot be used due to the high calculation cost. The objective of this study is to make the new semi-optimal control law for the minimum time attitude maneuver of the satellite equipped with the VSCMG. The new control law is designed using a rule-based feedforward control combined with feedback control. The result by numerical simulation has shown that the proposed control law enables the satellite to achieve faster maneuver without iterative calculations. </p>

    Other Link: https://ci.nii.ac.jp/naid/130008021251

  • Semi-Optimal Control for Minimum-Time Maneuver of Satellite with Variable Speed Pyramid Type SGCMGs

    TSUCHIYA Mitsuyoshi, HIGUCHI Takehiro

    TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN   19 ( 1 )   24 - 33   2021.1

    DOI CiNii

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    Language:English   Publishing type:Research paper (scientific journal)   Publisher:一般社団法人 日本航空宇宙学会   Joint Work  

    <p>This study explores the minimum-time attitude maneuver of satellites using Control Moment Gyros (CMG). The CMG system is able to generate high torque and run for longer term than other actuators. However, it is known that the singular input that cannot generate effective torque appears in the optimal control for the minimum-time maneuver of a rigid spacecraft with a pyramid type SGCMG system. In previous studies, a new system equipped with variable speed CMG (VSCMG) to the CMG where the singular input appeared has been proposed. It is shown that the new system can rotate faster than the normal pyramid type SGCMG system in the simulation based on the optimal control law. However, for applications in actual satellites, numerical optimization cannot be used due to the high calculation cost. The objective of this study is to make the new semi-optimal control law for the minimum time attitude maneuver of the satellite equipped with the SGCMG with the variable speed wheel. The new control law is designed using a rule-based feedforward control combined with feedback control. The result by numerical simulation has shown that the proposed control law enables the satellite to achieve faster maneuver without any initial assumptions.</p>

    Other Link: https://ci.nii.ac.jp/naid/130007965802

  • AR マーカによる画像ベースモデル推定を用いたスケーラ ブルなマルチロータ機システムの開発

    ⻘⽊ ⼤地, 樋⼝ 丈浩,長瀬 駿之介, 南原 光晴, 上野 誠也

    第58回⾶⾏機シンポジウム講演論文集   2020.11

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    Language:Japanese   Publishing type:Research paper (research society, symposium materials, etc.)   Joint Work  

  • ピラミッド型VSCMG搭載衛星の最短時間姿勢変更

    及川 航平,樋⼝ 丈浩,⼟屋 光慶,上野 誠也

    第63回宇宙科学技術連合講演会講演集   2020.10

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    Language:Japanese   Publishing type:Research paper (research society, symposium materials, etc.)   Joint Work  

  • Synchronizing Motion Control for Tumbling Space Debris Using Robotic Arm

    Takehiro Higuchi, Tomoaki Fujihara

    2020.9

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    Language:English   Publishing type:Research paper (international conference proceedings)   Joint Work  

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Awards 【 display / non-display

  • SICE-ICASE International Joint Conference 2006 Young Author Award

    2006.10    

  • ISTS Student Session JSASS President Award

    2002    

Grant-in-Aid for Scientific Research 【 display / non-display

  • Developement of High Torque Pyramid Type Micro VS-CMG Applying Singular Input

    2020.4

    Grant-in-Aid for Scientific Research  Grant-in-Aid for Scientific Research(C)

    Investigator(s):Takehiro Higuchi

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    Grant type:Competitive

  • Experiment on Control Conflict of Avoidance Manuvoer of Small UAV

    2007.4 - 2009.3

    Grant-in-Aid for Scientific Research  Grant-in-Aid for Young Scientists(B)

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    Grant type:Competitive

Past of Collaboration and Commissioned Research 【 display / non-display

  • SLIMプロジェクト

    Offer organization: JAXA/ISAS   Cooperative Research within Japan  

    Project Year: 2010.2  -   

  • UZUMEプロジェクト

    Offer organization: JAXA/ISAS   Cooperative Research within Japan  

    Project Year: 2020.12  -   

 

Charge of on-campus class subject 【 display / non-display

  • 2021   海洋宇宙システム工学演習B

    Graduate school of Engineering Science

  • 2021   海洋宇宙システム工学演習A

    Graduate school of Engineering Science

  • 2021   航空宇宙利用工学

    Graduate school of Engineering Science

  • 2021   空間利用工学

    Graduate School of Environment and Information Sciences

  • 2021   飛行ロボティクス設計

    College of Engineering Science

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Committee Memberships 【 display / non-display

  • 計測自動制御学会 航法誘導制御技術研究会 主査

    2019.1 

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    Committee type:Academic society 

  • 日本航空宇宙学会論文集 論文編集委員

    2017.4 - 2018.3 

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    Committee type:Academic society 

  • 計測自動制御学会 アドバンスト航法誘導制御技術研究会 幹事

    2016.12 - 2018.12 

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    Committee type:Academic society