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Feedback attitude control of spacecraft using two single gimbal control moment gyros

Advances in space research, 2021-10, Vol.68 (7), p.2713-2726

2021

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Stochastic stabilization of rigid body motion of a spacecraft on SE(3)

International journal of control, 2021-05, Vol.94 (5), p.1166-1173

2021

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Landing Guidance Control Combining Powered Descending with Nonlinear Optimization and Vertical Descending with Model Prediction

Journal of robotics and mechatronics, 2024-10, Vol.36 (5), p.1110-1121

2024

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Design and validation of an MPC controller for CMG-based testbed

Optimization and engineering, 2023-03, Vol.24 (1), p.185-221

2023

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Inverse Kinematics in Pyramid-Type Single-Gimbal Control Moment Gyro System

Journal of guidance, control, and dynamics, 2016-08, Vol.39 (8), p.1893-1903

2016

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Analytical expression for distant retrograde orbits around a small natural satellite

Advances in space research, 2019-02, Vol.63 (3), p.1336-1346

2019

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Directional passability and quadratic steering logic for pyramid-type single gimbal control moment gyros

Acta astronautica, 2014-09, Vol.102, p.103-123

2014

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Optimal Position and Attitude Control of Quadcopter Using Stochastic Differential Dynamic Programming with Input Saturation Constraints

Journal of robotics and mechatronics, 2021-04, Vol.33 (2), p.283-291

2021

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Selecting Initial Gimbal Angles of Roof-type CMG System for Avoiding Singularities in Spacecraft Attitude Maneuver

TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 2022, Vol.65(3), pp.123-133

2022

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Rate Damping of a Spacecraft Using Two Single-Gimbal Control Moment Gyros

Journal of guidance, control, and dynamics, 2013-11, Vol.36 (6), p.1606-1623

2013

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Study on fundamental properties of the spraying Ultra High Strength Fiber Reinforced Concrete cured at normal temperature

MATEC Web of Conferences, 2022, Vol.364, p.5016

2022

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Structure of distributed control system in Seimei telescope

SICE Journal of Control, Measurement, and System Integration, 2021-06, Vol.14 (2), p.111-118

2021

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Open-Loop System Identification of MIMO Integrator Model

SICE Journal of Control, Measurement, and System Integration, 2020, Vol.13(3), pp.73-76

2020

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Modeling of hydraulic support system for large structures

Transactions of the JSME (in Japanese), 2021, Vol.87(900), pp.21-00059-21-00059

2021

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Experimental validation of hydraulic support system for large structures

Transactions of the JSME (in Japanese), 2021, Vol.87(900), pp.21-00060-21-00060

2021

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Analysis of period-multiplying bifurcations of distant retrograde orbits in the Hill three-body problem

Advances in space research, 2022-11, Vol.70 (10), p.3016-3033

2022

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Simultaneous Learning Optimization of Hamiltonian Systems and Trajectory Tracking Around an Asteroid

Journal of guidance, control, and dynamics, 2020-02, Vol.43 (2), p.222-231

2020

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Attitude control experiment of a spinning spacecraft using only magnetic torquers

Advances in space research, 2023-06, Vol.71 (12), p.5386-5399

2023

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Smooth and continuous interplanetary trajectory design of spacecraft using iterative patched-conic method

Acta astronautica, 2021-08, Vol.185, p.58-69

2021

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Attitude maneuver of spacecraft with a variable-speed double-gimbal control moment gyro

Advances in space research, 2016-10, Vol.58 (7), p.1303-1317

2016

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Modelling and design of a coupled system of multiple hydraulic systems and large structures

Kikai Gakkai ronbunshū = Transactions of the Japan Society of Mechanical Engineers, 2024-10, Vol.90 (938), p.24-00132-24-00132

2024

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Optimal constellation design based on satellite ground tracks for Earth observation missions

Acta astronautica, 2023-06, Vol.207, p.1-9

2023

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Agile rest-to-rest attitude maneuvering of spacecraft using pyramid-type SGCMG based on iteratively recalculated optimal trajectory

Advances in space research, 2022-10, Vol.70 (7), p.1988-2012

2022

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Quasi-time-optimal steering law for low-thrust orbit transfer considering angular momentum and torque constraints

Acta astronautica, 2021-05, Vol.182, p.332-349

2021

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Minimum energy coplanar orbit transfer of geostationary spacecraft using time-averaged Hamiltonian

Acta astronautica, 2019-07, Vol.160, p.270-279

2019

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Feedback attitude control of spacecraft using two single gimbal control moment gyros

Stochastic stabilization of rigid body motion of a spacecraft on SE(3)

Landing Guidance Control Combining Powered Descending with Nonlinear Optimization and Vertical Descending with Model Prediction

Design and validation of an MPC controller for CMG-based testbed

Inverse Kinematics in Pyramid-Type Single-Gimbal Control Moment Gyro System

Analytical expression for distant retrograde orbits around a small natural satellite

Directional passability and quadratic steering logic for pyramid-type single gimbal control moment gyros

Optimal Position and Attitude Control of Quadcopter Using Stochastic Differential Dynamic Programming with Input Saturation Constraints

Selecting Initial Gimbal Angles of Roof-type CMG System for Avoiding Singularities in Spacecraft Attitude Maneuver

Rate Damping of a Spacecraft Using Two Single-Gimbal Control Moment Gyros

Study on fundamental properties of the spraying Ultra High Strength Fiber Reinforced Concrete cured at normal temperature

Structure of distributed control system in Seimei telescope

Open-Loop System Identification of MIMO Integrator Model

Modeling of hydraulic support system for large structures

Experimental validation of hydraulic support system for large structures

Analysis of period-multiplying bifurcations of distant retrograde orbits in the Hill three-body problem

Simultaneous Learning Optimization of Hamiltonian Systems and Trajectory Tracking Around an Asteroid

Attitude control experiment of a spinning spacecraft using only magnetic torquers

Smooth and continuous interplanetary trajectory design of spacecraft using iterative patched-conic method

Attitude maneuver of spacecraft with a variable-speed double-gimbal control moment gyro

Modelling and design of a coupled system of multiple hydraulic systems and large structures

Optimal constellation design based on satellite ground tracks for Earth observation missions

Agile rest-to-rest attitude maneuvering of spacecraft using pyramid-type SGCMG based on iteratively recalculated optimal trajectory

Quasi-time-optimal steering law for low-thrust orbit transfer considering angular momentum and torque constraints

Minimum energy coplanar orbit transfer of geostationary spacecraft using time-averaged Hamiltonian

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