SATOH Atsushi

写真a

Affiliation

IWATE University  Faculty of Science and Engineering  Department of Systems Innovation Engineering  Studies in Mechanical Science and Engineering 

Position

Associate Professor

Year of Birth

1971

Laboratory Address

〒0208551 Ueda 4-3-5, Morioka

Laboratory Phone number

+81-19-621-6404

Laboratory Fax number

+81-19-621-6404

Mail Address

E-mail address

Research Interests 【 display / non-display

  • Transient response shaping

  • Unmanned Aerial Vehicle

  • Flight control

  • LMI approach

  • Application of numerical optimization to control

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Graduate School 【 display / non-display

  •  
    -
    2000.03

    Nagoya University  Graduate School, Division of Engineering  Department of Aerospace Engineering  Doctor's Course  Accomplished Credits for Doctoral Program

  •  
    -
    1997.03

    Nagoya University  Graduate School, Division of Engineering  Department of Aerospace Engineering  Master's Course  Completed

Campus Career 【 display / non-display

  • 2007.04
    -
    Now

    IWATE University   Associate Professor   [Duty]

  • 2018.04
    -
    2020.03

    IWATE University   Faculty of Science and Engineering   [Concurrently]

  • 2014.04
    -
    2016.03

    IWATE University   Education Promotion Organization   Associate Professor   [Concurrently]

  • 2005.06
    -
    2007.03

    IWATE University   Lecturer   [Duty]

External Career 【 display / non-display

  • 2018.07
    -
    2019.06

    Japan Society for the Promotion of Science   Technical Advisor  

  • 2015.02
     
     

    Japan Aerospace Technology Foundation   Research Advisor  

  • 2000.04
    -
    2005.05

    Nara Institute of Science and Technology   Research Assistant  

Research Areas 【 display / non-display

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

  • Informatics / Mechanics and mechatronics

  • Manufacturing Technology (Mechanical Engineering, Electrical and Electronic Engineering, Chemical Engineering) / Control and system engineering

 

Course Subject 【 display / non-display

  • 2005

    English Seminar for Science and technology

  • 2005

    Control Engineering

  • 2005

    Analytical Dynamics

  • 2006

  • 2006

    Exercises on Mechanical Vibrations

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Published Papers 【 display / non-display

  • ENDURANCE ANALYSIS OF BATTERY-POWERED MULTICOPTERS: DERIVATION OF PROPER CUT-OFF VOLTAGE USING DC MOTOR MODEL

    A. Satoh, M. Watanabe, K. Hozumi, A. Watanabe

    Proceedings of ICAS 2020/2021 ( International council of the aeronautical sciences (ICAS) )    2021.11  [Refereed]

    Others  Multiple authorship

  • ANALYSIS OF AERODYNAMIC CHARACTERISTICS OF PROPELLER AT LOW ADVANCE RATIO USING A WHIRING ARM

    Y. Itoh, A. Satoh

    Proceedings of ICAS 2020/2021 ( International council of the aeronautical sciences (ICAS) )    2021.11  [Refereed]

    Others  Multiple authorship

  • Modeling and Numerical Investigation of Aerodynamic Characteristics of a Propeller Circling on a Whirling Arm

    Y. Itoh, A. Satoh

    Transactions of the Japan Society for Aeronautical and Space Sciences ( JSASS )  64 ( 6 ) 335 - 347   2021.06  [Refereed]

    Bulletin of University, Institute, etc.  Multiple authorship

  • Derivation of Discharge Cut-off Condition in Hovering Flight Using DC Motor Equivalent Circuit Model and Hover Endurance Analysis of Multicopters

    Journal of the Japan Society for Aeronautical and Space Sciences ( JSASS )  68 ( 2 ) 57 - 64   2020.04  [Refereed]

    Academic Journal  Multiple authorship

    Recentry, there is a strong demand for endurance improvement of multicopters with electric propulsion
    system. As for the hover endurance, it mainly depends on the power consumption and the effective battery capacity in
    hover condition. In this work, the motor operating condition for hovering is derived from propeller characteristic and DC
    motor equivalent circuit model. Using these conditions, new discharge cut-off conditions which enable us to determine
    the proper effective capacity in hovering flight are derived. The hover endurance analysis according to the estimated
    effective capacity is discussed. The parametric study of hover endurance with respect to the takeoff weight and the
    battery weight to payload ratio is shown for a model quadcopter.

  • Measurement of Propeller Characteristics at a Negative Advance Ratio Using a Whirling Arm Facility

    Y. Itoh, A. Satoh

    Lecture Notes in Electrical Engineering: The Proceedings of the 2018 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2018) ( Springer )    1169 - 1188   2019.06  [Refereed]

    Others  Multiple authorship

    DOI

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Presentations 【 display / non-display

  • Observer-based propeller torque estimation based on polynomial motor torque model

    Oral Presentation(General)  Naoto Abe, Kohei Ono, Atsushi Satoh

    2021.05
     
     

  • Two-dimensional ultrasonic airspeed measurement based on phase-shift method without requiring knowledge of the speed of sound

    Oral Presentation(General)  Tomohide Tanaka, Hirofumi Kumagai, Atsushi Satoh

    2021.05
     
     

  • Development of vertical catamaran airship -Weight saving and construction of flight data acquisition system-

    Oral Presentation(General) 

    2021.03
     
     

  • Development of vertical catamaran airship -Weight saving and construction of flight data acquisition system-

    Oral Presentation(General)  Akisuke Katok, Kazuyuki Ueno, Atsushi Sato

    2020.03
     
     

  • Measurement of Propeller Characteristics at a Negative Advance Ratio Using a Whirling Arm Facility

    Oral Presentation(General)  Yuto Itoh, Atsushi Satoh

    2018.10
     
     

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Academic Awards Received 【 display / non-display

  • 2014.05.19

  • 2013.05.29

  • 2008.05

Association Memberships 【 display / non-display

  • 2016.03
     
     
     

    IJCAS

Academic Activity 【 display / non-display

  • 2016.03
    -
    2019.03

    IJCAS