TY - GEN
T1 - Dynamics and control of flexible manipulators using variable-speed control moment gyros
AU - Hu, Quan
AU - Wang, Zhaohui
AU - Zhang, Jingrui
N1 - Publisher Copyright:
© 2015, E-flow American Institute of Aeronautics and Astronautics (AIAA). All rights reserved.
PY - 2015
Y1 - 2015
N2 - In this paper, the variable-speed control moment gyros (VS-CMGs) are adopted as actuators for vibration suppression of space flexible manipulators. They are directly mounted on the flexible links of the manipulator. Such system can be viewed as a flexible multibody system in chain topology actuated by both joint motors and VS-CMGs. We first develop a general approach for establishing the system equations of motion through Kane’s method. Then, two controllers are designed for trajectory tracking and vibration suppression of the flexible manipulator: one is an inverse dynamics control, whereas the other is based on the singular perturbation method. The proposed two control strategies are applied to a free-flying platform with a flexible manipulator. Numerical results show that the VS-CMGs can significantly suppress the induced vibration of the flexible links during the large angle maneuver.
AB - In this paper, the variable-speed control moment gyros (VS-CMGs) are adopted as actuators for vibration suppression of space flexible manipulators. They are directly mounted on the flexible links of the manipulator. Such system can be viewed as a flexible multibody system in chain topology actuated by both joint motors and VS-CMGs. We first develop a general approach for establishing the system equations of motion through Kane’s method. Then, two controllers are designed for trajectory tracking and vibration suppression of the flexible manipulator: one is an inverse dynamics control, whereas the other is based on the singular perturbation method. The proposed two control strategies are applied to a free-flying platform with a flexible manipulator. Numerical results show that the VS-CMGs can significantly suppress the induced vibration of the flexible links during the large angle maneuver.
UR - http://www.scopus.com/inward/record.url?scp=84973509192&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:84973509192
T3 - AIAA Guidance, Navigation, and Control Conference 2015, MGNC 2015 - Held at the AIAA SciTech Forum 2015
BT - AIAA Guidance, Navigation, and Control Conference 2015, MGNC 2015 - Held at the AIAA SciTech Forum 2015
PB - American Institute of Aeronautics and Astronautics Inc.
T2 - AIAA Guidance, Navigation, and Control Conference 2015, MGNC 2015 - Held at the AIAA SciTech Forum 2015
Y2 - 5 January 2015 through 9 January 2015
ER -