379 results on '"Yamada, Katsuhiko"'
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2. Design and validation of an MPC controller for CMG-based testbed
3. Attitude control experiment of a spinning spacecraft using only magnetic torquers
4. Optimal constellation design based on satellite ground tracks for Earth observation missions
5. Analysis of period-multiplying bifurcations of distant retrograde orbits in the Hill three-body problem
6. Agile rest-to-rest attitude maneuvering of spacecraft using pyramid-type SGCMG based on iteratively recalculated optimal trajectory
7. Feedback attitude control of spacecraft using two single gimbal control moment gyros
8. Smooth and continuous interplanetary trajectory design of spacecraft using iterative patched-conic method
9. Quasi-time-optimal steering law for low-thrust orbit transfer considering angular momentum and torque constraints
10. Development of a cold chopper for TAO/MIMIZUKU: onboard test on MIMIZUKU
11. Development of a cold chopper for TAO/MIMIZUKU: repetitive control
12. Attitude control for spacecraft using pyramid-type variable-speed control moment gyros
13. Minimum energy coplanar orbit transfer of geostationary spacecraft using time-averaged Hamiltonian
14. Analytical expression for distant retrograde orbits around a small natural satellite
15. Study on fundamental properties of the spraying Ultra High Strength Fiber Reinforced Concrete cured at normal temperature
16. Attitude maneuver of spacecraft with a variable-speed double-gimbal control moment gyro
17. Approximating elliptic halo orbits based on the variation of constants
18. Development of a cold chopper for TAO/MIMIZUKU: Cryogenic test
19. Directional passability and quadratic steering logic for pyramid-type single gimbal control moment gyros
20. State transition matrix for long-distance formation with J2 in eccentric orbits
21. 地球観測衛星のためのグランドトレース配置を考慮した最適コンステレーション設計
22. Minimum Time Attitude Maneuver of Spacecraft with Flexible Structures
23. Study on fundamental properties of the spraying Ultra High Strength Fiber Reinforced Concrete cured at normal temperature.
24. Fuel-optimal eccentricities for precise formation keeping of spacecraft on Keplerian orbits
25. Control Performance Analysis of Centralized Control System in the Seimei Telescope
26. Selecting Initial Gimbal Angles of Roof-type CMG System for Avoiding Singularities in Spacecraft Attitude Maneuver
27. Design of Periodic Orbits for Formation Flying around a Halo Orbit
28. 磁気トルカによるスピン衛星の姿勢制御実験
29. Structure of distributed control system in Seimei telescope
30. Design and validation of an MPC controller for CMG-based testbed
31. Spacecraft Formation Design and Control in Keplerian Elliptic Orbits
32. ルーフ配置型CMGによる宇宙機の最適姿勢変更計画
33. 宇宙機のピラミッド配置型CMGによる最適姿勢制御と実験
34. Impulsive control for angular momentum management of tumbling spacecraft
35. Control of Dual-Spin Turn of Spacecraft
36. Optimal Earth-Moon Transfer Trajectory Design via Differential Dynamic Programming with Input Saturation Constraints
37. Modeling of hydraulic support system for large structures
38. Stability Analysis of Spacecraft Motion in the Vicinity of a Second Body in the Elliptic Restricted Three-body Problem
39. Stochastic Bounded Stability in the Three-Body Problem with Probabilistic Uncertainty Using Port-Hamiltonian Representation
40. Experimental validation of hydraulic support system for large structures
41. Optimized Planning Method of Earth Imaging by a Spacecraft with CMGs
42. Attitude Rate Damping Control of a Stratospheric Balloon Gondola with CMGs
43. Semi-Optimal Steering Logic of Low-Thrust Orbit Raising Considering Angular Momentum Constraint
44. Development status of the segmented mirror control system in Seimei Telescope
45. Development of a cold chopper for TAO/MIMIZUKU
46. Development of a cold chopper for TAO/MIMIZUKU: cryogenic test
47. Open-Loop System Identification of MIMO Integrator Model
48. Simultaneous Learning Optimization of Hamiltonian Systems and Trajectory Tracking Around an Asteroid
49. Optimization of Low-Thrust Transfer Trajectories to L1 and L2 Halo Orbits in the Earth-Moon System
50. Attitude Control of a Spinning Spacecraft Using Only Magnetic Torquers
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