INAMORI Takaya 稲守孝哉

… Alternative Names

Researcher Number	50725249
Other IDs
Affiliation (Current)	2020: 名古屋大学, 工学研究科, 准教授
Affiliation (based on the past Project Information) *help	2020: 名古屋大学, 工学研究科, 准教授 2016 – 2018: 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 Aerospace engineering / Basic Section 24010:Aerospace engineering-related / Medium-sized Section 24:Aerospace engineering, marine and maritime engineering, and related fields
Keywords	Principal Investigator 小型衛星 / 軌道制御 / フォーメーションフライト / 姿勢外乱トルク / 宇宙機姿勢制御 / 軌道力学 / 宇宙構造物

Development of orbital mechanics from discrete system to continuous system for space flexible structurePrincipal InvestigatorOngoing
- Principal Investigator
  
  稲守孝哉
- 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 InvestigatorOngoing
- Principal Investigator
  
  稲守孝哉
- 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 2018 2017 2015

All Journal Article Presentation

[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 Pages: 2010-2021
- DOI
  10.1016/j.asr.2018.01.038
- Peer Reviewed
- Data Source
  KAKENHI-PROJECT-15K18281
[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: 1 results

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

# of Collaborated Projects: 1 results

# of Collaborated Products: 0 results
3. MATSUZAWA Shinji

# of Collaborated Projects: 1 results

# of Collaborated Products: 2 results
4. FUJIWARA Masaki

# of Collaborated Projects: 1 results

# of Collaborated Products: 0 results

INAMORI Takaya 稲守 孝哉

稲守 孝哉 イナモリ タカヤ

INAMORI TAKAYA 稲守 孝哉

Research Projects

Research Products

Co-Researchers

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

Principal Investigator

Project Period (FY)

Research Category

Review Section

Research Institution

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

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

Author(s)

Journal Title

DOI

Data Source

[Presentation] Propellantless Close Range Rendezvous and Docking Using a Single Electromagnetic Device for Small Spacecraft2018

Author(s)

Organizer

Data Source

[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)

Organizer

Data Source

[Presentation] Particle Simulation of Interactions between Plasma and Magnetic Field Surrounding Nanosatellite Magnetic Torquers2015

Author(s)

Organizer

Place of Presentation

Year and Date

Data Source

INAMORI Takaya 稲守孝哉

稲守孝哉イナモリタカヤ

INAMORI TAKAYA 稲守孝哉