INAMORI Takaya 稲守孝哉

… Alternative Names

INAMORI TAKAYA 稲守孝哉

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Researcher Number	50725249
Other IDs
Affiliation (Current)	2025: 名古屋大学, 工学研究科, 准教授
Affiliation (based on the past Project Information) *help	2020 – 2024: 名古屋大学, 工学研究科, 准教授 2016 – 2019: 名古屋大学, 工学研究科, 講師 2017: 名古屋大学, 大学院工学研究科, 講師 2015: 東京大学, 工学(系)研究科(研究院), 助教
Review Section/Research Field	Principal Investigator Basic Section 24010:Aerospace engineering-related / Medium-sized Section 24:Aerospace engineering, marine and maritime engineering, and related fields / Aerospace engineering
Keywords	Principal Investigator 軌道力学 / 軌道制御 / 軌道運動 / 宇宙プラズマ / 宇宙構造物 / 人工衛星 / 小型衛星 / 帯電 / 姿勢運動 / 磁気トルカ … More / 軌道力 / 宇宙機姿勢制御 / 姿勢外乱トルク / 磁気トルク / 剛体姿勢運動 / フォーメーションフライト Less

Satellite orbit control utilizing charging phenomena resulting from differences in ion-electron magnetization induced by satellite magnetic fieldsPrincipal Investigator
- Principal Investigator
  
  稲守孝哉
- Project Period (FY)
  2024 – 2026
- Research Category
  
  Grant-in-Aid for Scientific Research (B)
- Review Section
  
  Basic Section 24010:Aerospace engineering-related
- Research Institution
  Nagoya University
High-accurate relative position and rotation control of multiple satellites considering orbit-attitude coupled dynamics for space interferometryPrincipal Investigator
- Principal Investigator
  
  稲守孝哉
- Project Period (FY)
  2022 – 2024
- Research Category
  
  Grant-in-Aid for Challenging Research (Exploratory)
- Review Section
  
  Medium-sized Section 24:Aerospace engineering, marine and maritime engineering, and related fields
- Research Institution
  Nagoya University
Ion-scale interactions between space plasma and satellite magnetic fields targeting orbit controlPrincipal Investigator
- Principal Investigator
  
  Inamori Takaya
- Project Period (FY)
  2021 – 2023
- Research Category
  
  Grant-in-Aid for Scientific Research (B)
- Review Section
  
  Basic Section 24010:Aerospace engineering-related
- Research Institution
  Nagoya University
Development of orbital mechanics from discrete system to continuous system for space flexible structurePrincipal Investigator
- Principal Investigator
  
  Inamori Takaya
- Project Period (FY)
  2020 – 2021
- Research Category
  
  Grant-in-Aid for Challenging Research (Exploratory)
- Review Section
  
  Medium-sized Section 24:Aerospace engineering, marine and maritime engineering, and related fields
- Research Institution
  Nagoya University
Accurate attitude control in small satellites by disturbance compensation considering scale dependencyPrincipal Investigator
- Principal Investigator
  
  Inamori Takaya
- Project Period (FY)
  2018 – 2019
- Research Category
  
  Grant-in-Aid for Early-Career Scientists
- Review Section
  
  Basic Section 24010:Aerospace engineering-related
- Research Institution
  Nagoya University
Formation flight using plasma drag force generated by an electromagnetic coil for small satellitesPrincipal Investigator
- Principal Investigator
  
  INAMORI TAKAYA
- Project Period (FY)
  2015 – 2017
- Research Category
  
  Grant-in-Aid for Young Scientists (B)
- Research Field
  
  Aerospace engineering
- Research Institution
  Nagoya University
  The University of Tokyo

All 2023 2022 2021 2020 2019 2018 2017 2015

All Journal Article Presentation

[Journal Article] Attitude Control of Spin-type Membrane Structures using Electromagnetic Force in Earth Orbit2022
- Author(s)
  Y. Yamada, T. Inamori, J. H. Park, Y. Satou, Y. Sugawara, and K. Yamaguchi
- Journal Title
  
  Advances in Space Research
  
  Volume: 69-10 Issue: 10 Pages: 3864-3879
- DOI
  10.1016/j.asr.2022.02.050
- Peer Reviewed
- Data Source
  KAKENHI-PROJECT-20K21045
[Journal Article] Electromagnetic Deployment of a Membrane Structure in LEO2021
- Author(s)
  山田裕己，稲守孝哉，佐藤泰貴，川井翼，菅原佳城
- Journal Title
  
  JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
  
  Volume: 69 Issue: 5 Pages: 187-196
- DOI
  10.2322/jjsass.69.187
- NAID
  130008101384
- ISSN
  1344-6460, 2432-3691
- Language
  Japanese
- Peer Reviewed
- Data Source
  KAKENHI-PROJECT-20K21045
[Journal Article] Magnetic attitude disturbance caused by asymmetrical magnetic substances in LEO satellites2019
- Author(s)
  T. Inamori, P. Saisutjarit, N. Sako, Y. Terao, and S. Nakasuka
- Journal Title
  
  Journal of Aerospace Engineering
  
  Volume: 32-6 Issue: 6 Pages: 1-12
- DOI
  10.1061/(asce)as.1943-5525.0001082
- Peer Reviewed
- Data Source
  KAKENHI-PROJECT-18K13924
[Journal Article] Nanosatellite constellation deployment using on-board magnetic torquer interaction with space plasma2018
- Author(s)
  J. Park, S. Matsuzawa, T. Inamori, I. Jeung
- Journal Title
  
  Advances in space research
  
  Volume: 61-8 Issue: 8 Pages: 2010-2021
- DOI
  10.1016/j.asr.2018.01.038
- Peer Reviewed
- Data Source
  KAKENHI-PROJECT-15K18281
[Presentation] Attitude Control of Spacecraft with Membrane Using Interplanetary Magnetic Field with Consideration of Vibration2023
- Author(s)
  Hoang Xuan Truong An, T. Inamori
- Organizer
  The 34th International Symposium on Space Technology and Science
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-22K18856
[Presentation] Patched bang-bang control for spacecraft attitude stabilization during magnetic plasma drag in-orbit demonstration2023
- Author(s)
  Park Ji Hyun, 稲守孝哉, 宇佐見海渡, 吉川英儀, 山口皓平 , 川嶋嶺
- Organizer
  第67回宇宙科学連合講演会
- Data Source
  KAKENHI-PROJECT-21H01531
[Presentation] Drag Force Augmentation of Magnetic Plasma Deorbit Method for Nanosatellites2023
- Author(s)
  R. Kameyama, R. Kawashima, and T. Inamori
- Organizer
  Plasma Application and Hybrid Functionally Materials
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-21H01531
[Presentation] Magnetic plasma drag demonstration mission for nanosatellite orbit control2022
- Author(s)
  J. Park, T. Inamori, H. Masuda, T. Miyamoto, T. Noro, K. Nagai, K. Kinefuchi, R. Kawashima, K. Yamaguchi
- Organizer
  The 33rd International Symposium on Space Technology and Science
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-21H01531
[Presentation] 姿勢・軌道の連成振動を考慮した宇宙用伸展ブームの挙動解析2022
- Author(s)
  坂口友太，稲守孝哉，山口皓平
- Organizer
  第66回宇宙科学技術連合講演会
- Data Source
  KAKENHI-PROJECT-22K18856
[Presentation] 宇宙プラズマと磁気トルカの相互作用による現象を用いた小型宇宙機の軌道制御への応用2022
- Author(s)
  宮本岳瑠, 稲守孝哉, Ji Hyun Park, 川嶋嶺
- Organizer
  第66回宇宙科学技術連合講演会
- Data Source
  KAKENHI-PROJECT-21H01531
[Presentation] 磁気トルカと地球低軌道プラズマの相互作用から生じる力の実験研究2021
- Author(s)
  増田裕明，稲守孝哉，Park Ji Hyun，川嶋嶺，杵淵紀世志，山口皓平
- Organizer
  第65回宇宙科学技術連合講演会
- Data Source
  KAKENHI-PROJECT-21H01531
[Presentation] 柔軟構造物の軌道運動効果を考慮した相対位置・姿勢の超高精度化2020
- Author(s)
  中山理志，稲守孝哉，山田裕己
- Organizer
  第64回宇宙科学技術連合講演会
- Data Source
  KAKENHI-PROJECT-20K21045
[Presentation] A fuel-free and agile attitude maneuver of space membrane structures using electromagnetic force in LEO2019
- Author(s)
  Y. Yamada, T. Inamori, Y. Satou
- Organizer
  The 70th International Astronautical Congress
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-18K13924
[Presentation] Propellantless Close Range Guidance and Docking for Small Satellites using Simple Electromagnetic Devices2019
- Author(s)
  Y. Yamada, T. Inamori
- Organizer
  The 32nd International Symposium on Space Technology and Science
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-18K13924
[Presentation] Propellantless Close Range Rendezvous and Docking Using a Single Electromagnetic Device for Small Spacecraft2018
- Author(s)
  Y. Yamada, T. Inamori, M. Tomooka
- Organizer
  The 69th International Astronautical Congress
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-18K13924
[Presentation] 超小型衛星における宇宙プラズマ抗力を用いたデオービット2017
- Author(s)
  松澤真司，稲守孝哉，川嶋嶺，尾崎直哉
- Organizer
  第61回宇宙科学技術連合講演会
- Data Source
  KAKENHI-PROJECT-15K18281
[Presentation] Particle Simulation of Interactions between Plasma and Magnetic Field Surrounding Nanosatellite Magnetic Torquers2015
- Author(s)
  R. Kawashima, T. Inamori, T. Matsuguma
- Organizer
  The 30th International Symposium on Space Technology and Science (ISTS)
- Place of Presentation
  兵庫県・神戸市・神戸コンベンションセンター
- Year and Date
  2015-07-04
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-15K18281

1. KAWASHIMA Rei (80794429)

# of Collaborated Projects: 3 results

# of Collaborated Products: 7 results
2. 杵淵紀世志 (90648502)

# of Collaborated Projects: 2 results

# of Collaborated Products: 2 results
3. 佐藤泰貴 (70726760)

# of Collaborated Projects: 1 results

# of Collaborated Products: 1 results
4. MATSUZAWA Shinji

# of Collaborated Projects: 1 results

# of Collaborated Products: 2 results
5. FUJIWARA Masaki

# of Collaborated Projects: 1 results

# of Collaborated Products: 0 results

INAMORI Takaya 稲守 孝哉

INAMORI TAKAYA 稲守 孝哉

Research Projects

Research Products

Co-Researchers

Satellite orbit control utilizing charging phenomena resulting from differences in ion-electron magnetization induced by satellite magnetic fieldsPrincipal Investigator

Principal Investigator

Project Period (FY)

Research Category

Review Section

Research Institution

High-accurate relative position and rotation control of multiple satellites considering orbit-attitude coupled dynamics for space interferometryPrincipal Investigator

Principal Investigator

Project Period (FY)

Research Category

Review Section

Research Institution

Ion-scale interactions between space plasma and satellite magnetic fields targeting orbit controlPrincipal Investigator

Principal Investigator

Project Period (FY)

Research Category

Review Section

Research Institution

Development of orbital mechanics from discrete system to continuous system for space flexible structurePrincipal Investigator

Principal Investigator

Project Period (FY)

Research Category

Review Section

Research Institution

Accurate attitude control in small satellites by disturbance compensation considering scale dependencyPrincipal Investigator

Principal Investigator

Project Period (FY)

Research Category

Review Section

Research Institution

Formation flight using plasma drag force generated by an electromagnetic coil for small satellitesPrincipal Investigator

Principal Investigator

Project Period (FY)

Research Category

Research Field

Research Institution

[Journal Article] Attitude Control of Spin-type Membrane Structures using Electromagnetic Force in Earth Orbit2022

Author(s)

Journal Title

DOI

Data Source

[Journal Article] Electromagnetic Deployment of a Membrane Structure in LEO2021

Author(s)

Journal Title

DOI

NAID

ISSN

Language

Data Source

[Journal Article] Magnetic attitude disturbance caused by asymmetrical magnetic substances in LEO satellites2019

Author(s)

Journal Title

DOI

Data Source

[Journal Article] Nanosatellite constellation deployment using on-board magnetic torquer interaction with space plasma2018

Author(s)

Journal Title

DOI

Data Source

[Presentation] Attitude Control of Spacecraft with Membrane Using Interplanetary Magnetic Field with Consideration of Vibration2023

Author(s)

Organizer

Data Source

[Presentation] Patched bang-bang control for spacecraft attitude stabilization during magnetic plasma drag in-orbit demonstration2023

Author(s)

Organizer

Data Source

[Presentation] Drag Force Augmentation of Magnetic Plasma Deorbit Method for Nanosatellites2023

Author(s)

Organizer

Data Source

[Presentation] Magnetic plasma drag demonstration mission for nanosatellite orbit control2022

Author(s)

Organizer

Data Source

INAMORI Takaya 稲守孝哉

INAMORI TAKAYA 稲守孝哉