Research keywords (3):
spacecraft
, Space Debris
, Satellite
Research theme for competitive and other funds (5):
2004 - 2005 テープ型のテザーによる超小型衛星の落下促進の研究
スペースデブリの研究
超小型人工衛星の開発
Space Debris
Development of Small Satellite
Papers (23):
Yutaka Terao, Hiroshi Hirayama, Hirotaka Sugawara, Hitoshi Oyori. Electromagnetic Design of Dual Winding Permanent Magnet Synchronous Motor for Electromechanical Actuators of Flight Control Systems. 2022 International Power Electronics Conference (IPEC-Himeji 2022- ECCE Asia). 2022. 2135-2140
Masayuki KATAYAMA, Shinji HOKAMOTO, Shigeru ASO, Hiroshi HIRAYAMA. Study on Deorbit of a Microsatellite Considering the Solar Activity Effect on Atmospheric Density. AEROSPACE TECHNOLOGY JAPAN, THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 2020. 19. 47-55
Masayuki Katayama, Yuta Suzaki, Shigeru Aso, Hiroshi Hirayama. Attitude Control Simulator for the Small Satellite and Its Validation by On-orbit Data of QSAT-EOS. AIAA/USU Conference on Small Satellites. 2017
Ieyoung Kim, Toshiya Hanada, Hiroshi Hirayama. Success rate and effect of using electrodynamic tether system for de-orbit leo spacecraft. 60th International Astronautical Congress 2009, IAC 2009. 2009. 3. 1870-1879