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Publications by Takashi Shimomura
Stabilization of a Spacecraft With Control Moment Gyros
Transactions of the Institute of Systems, Control and Information Engineers
New Lipophilic Fluorescent Dyes for Exosome Labeling: Monitoring of Cellular Uptake of Exosomes
Effect of Size, Age and Division of Tuber on the Growth of Oxalis Articulata Savigny.
Journal of the Japanese Society of Revegetation Technology
Related publications
Optimal Attitude Control for Spacecraft Using Two Variable-Speed Control Moment Gyros
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
A Practical Rapid Attitude Maneuver Control System Using Control Moment Gyros for Microsatellite TSUBAME
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
Attitude-Tracking Control With Path Planning for Agile Satellite Using Double-Gimbal Control Moment Gyros
Mathematical Problems in Engineering
Mathematics
Engineering
Singularity Avoidance of Control Moment Gyros by Predicted Singularity Robustness: Ground Experiment
IEEE Transactions on Control Systems Technology
Control
Systems Engineering
Electrical
Electronic Engineering
Robust Finite Time Control for Stabilization of Rigid Spacecraft
Spacecraft Adaptive Attitude and Power Tracking With Variable Speed Control Moment Gyroscopes
Journal of Guidance, Control, and Dynamics
Control
Systems Engineering
Electronic Engineering
Applied Mathematics
Space
Electrical
Planetary Science
Aerospace Engineering
Steering Law of Control Moment Gyros Using Optimization of Initial Gimbal Angles for Satellite Attitude Control
Nippon Kikai Gakkai Ronbunshu, C Hen/Transactions of the Japan Society of Mechanical Engineers, Part C
Mechanics of Materials
Industrial
Mechanical Engineering
Manufacturing Engineering
A Robust Optimization Approach for Magnetic Spacecraft Attitude Stabilization
Journal of Optimization Theory and Applications
Control
Management Science
Applied Mathematics
Optimization
Operations Research
Time-Varying Feedback Stabilization of the Attitude of a Rigid Spacecraft With Two Controls
