DEVELOPMENT OF NANOSATELLITE FOR MOTHERSHIP DAUGHTERSHIP EXPERIMENT BY JAPANESE UNIVERSITIES
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概要
- 論文の詳細を見る
- 2000-03-01
著者
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MITSUHASHI Ryuichi
Hokkaido Institute of Technology
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SATORI Shin
Hokkaido Institute of Technology
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Satori S
Department Of Electric Electronics Engineering Hokkaido Institute Of Technology
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TAKEZAWA Satoshi
Hokkaido Institute of Technology
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NAGATA Atsushi
Advanced Technology Institute Ltd.
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ISHIKAWA Tomohiro
Hokkaido Institute of Technology
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NAKASUKA Shinichi
University of Tokyo
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OKAMOTO Hiroyuki
Astro Research Corporation
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Ishikawa Tomohiro
Graduate School Of Mechanical Systems Engineering Hokkaido Institute Of Technology
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Takezawa Satoshi
Mechanical System Engineering Hokkaido Institute Of Technology
関連論文
- Orbital Experiment of Nano-satellite "HIT-SAT" as a Sub-payload of M-V Rocket
- ATTITUDE CONTROL OF A MICRO SATELLITE WITH EVENTUAL SLIDING MODE CONTROLLER
- DEVELOPMENT OF NANOSATELLITE FOR MOTHERSHIP DAUGHTERSHIP EXPERIMENT BY JAPANESE UNIVERSITIES
- Results of the MicroLabSat project(Small satellite (2), Workshop for Space, Aeronautical and Navigational Electronics (W S A N E 2005))
- Results of the MicroLabSat project
- SB-8-5 In-orbit Demonstration of Orbital Maintenance System Using COTS Technologies(Small Satellite 1)(SB-8. Results of Various Satellite Missions)
- Preliminary experiments on technologies for satellite orbital maintenance using Micro-LabSat 1
- Experimental Investigation of Carbon Contamination Inside Discharge Chamber of Ion Thruster
- A reinforcement learning approach to fail-safe design for multiple space robots : cooperation mechanism without communication and negotiation schemes
- COMBUSTION CHARACTERISTICS OF FIBROUS FUELS FOR DRY TOWEL HYBRID ROCKET MOTOR
- Organizational learning model for adaptive collective behaviors in multiple robots
- THE CONTROL OF THE POWDER BODY PARTICLES APPLIED VOIGT MODEL
- Numerical Analysis of a Radiation-Cooled Micro Arcjet Thruster
- Numerical Analysis of the Rarefied Plume from an Arcjet Thruster: Effect of the Nozzle Exit Shape
- Outline of Mission and Development of Hodoyoshi Micro Satellites(Technical Session,ICSANE 2011(International Conference on Space, Aeronautical and Navigational Electronics 2011))