16 results on '"Nakasuka, Shinichi"'
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2. Command-centric architecture (C2A): Satellite software architecture with a flexible reconfiguration capability
3. Discussions on attitude determination and control system for micro/nano/pico-satellites considering survivability based on Hodoyoshi-3 and 4 experiences
4. Integral design method for simple and small Mars lander system using membrane aeroshell
5. Three-axis attitude control by two-step rotations using only magnetic torquers in a low Earth orbit near the magnetic equator
6. Magnetic dipole moment estimation and compensation for an accurate attitude control in nano-satellite missions
7. Evolution from education to practical use in University of Tokyo's nano-satellite activities
8. Structure and thermal control of panel extension satellite (PETSAT)
9. Rocket experiment on microwave power transmission with Furoshiki deployment
10. A satellite for demonstration of Panel Extension Satellite (PETSAT)
11. Technology demonstration on University of Tokyo's pico-satellite “XI-V” and its effective operation result using ground station network
12. Sounding rocket flight experiment for demonstrating “Furoshiki Satellite” for large phased array antenna
13. Large membrane “Furoshiki Satellite” applied to phased array antenna and its sounding rocket experiment
14. New attitude motion following control algorithm for capturing tumbling object in space
15. “Furoshiki satellite” - a large membrane structure as a novel space system
16. Cansat suborbital launch experiment-university educational space program using can sized pico-satellite
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