30 results on '"Hanada, Toshiya"'
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2. Improved contactless attitude control law of uncooperative spacecraft by laser ablation
3. Evaluation of the effectiveness of the 5-year rule — impact on the orbital environment at each altitude by reducing the post-mission disposal lifetime
4. Origin identification of sub-millimeter-sized debris from in-situ debris measurements
5. The impact assessment of accidental explosions of large constellations on low earth orbit environment
6. Considerations on the lists of the top 50 debris removal targets
7. Contactless attitude control of an uncooperative satellite by laser ablation
8. Assessing Collision Probability in Low-Thrust Deorbit
9. Space solar power satellite for the Moon and Mars mission
10. The collision avoidance strategy for geostationary satellites considering orbit maintenance
11. Impact on collision probability by post mission disposal and active debris removal
12. Estimation of orbital parameters of broken-up objects from in-situ debris measurements
13. Precise time estimation of on-orbit satellite fragmentations
14. An environmental estimation model for in-situ measurements of small space debris
15. Removal targets' classification: How time considerations modify the definition of the index
16. Simultaneous detection of multiple debris via a cascade of numerical evaluations and a voting scheme for lines in an image sequence
17. Orbital plane constraint applicable for in-situ measurement of sub-millimeter-size debris
18. Phasing Delta-V for transfers from Sun–Earth halo orbits to the Moon
19. Orbital objects detection algorithm using faint streaks
20. An orbit determination from debris impacts on measurement satellites
21. Development of in-situ micro-debris measurement system
22. Orbit determination by genetic algorithm and application to GEO observation
23. Storm-time atmospheric density modeling using neural networks and its application in orbit propagation
24. Practical method to identify orbital anomaly as spacecraft breakup in the geostationary region
25. Observation campaign dedicated to 1968-081E fragments identification
26. Benefits and risks of using electrodynamic tethers to de-orbit spacecraft
27. Searching for lost fragments in GEO
28. Stochastic analysis of survivability of double tether
29. Are de-orbiting missions possible using electrodynamic tethers? Task review from the space debris perspective
30. LOW-VELOCITY PROJECTILE IMPACT ON SPACECRAFT
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