TY - GEN
T1 - Simulation and Verification Platform for Three-Axis Air Bearing Table with CMG
AU - Qiao, Xin
AU - Jiang, Linghai
AU - Guo, Jiahua
AU - Shao, Zhijie
AU - Ma, Guangcheng
AU - Xia, Hongwei
N1 - Publisher Copyright:
© 2023 Technical Committee on Control Theory, Chinese Association of Automation.
PY - 2023
Y1 - 2023
N2 - This paper proposes a method to build a full physical simulation test platform, which can be used as a simulation and verification platform for three-axis air bearing table with the control moment gyro (CMG). To overcome the deficiency of being trapped in the momentum saturation singularities, a new steering logic based on a mixed weighted two-norm and least squares optimization solution is presented. To reduce the torque output pressure of CMG system, a switching logic is designed for the hybrid actuators, and the cold air thruster system is proposed for the requirements of large torque to reduce the probability of singularity and CMG is selected for high-precision smooth. To obtain fast and high-precision control effect, ADRC is presented to control the three-axis air bearing table. The results show that the system can reach stabilization rapidly, the error and the attitude stability can reach a good level, effectively protecting the single gimbal control moment gyro (SGCMG) system from singular state, making full use of the system's capabilities, and verifying the validity of the hybrid actuators switching logic.
AB - This paper proposes a method to build a full physical simulation test platform, which can be used as a simulation and verification platform for three-axis air bearing table with the control moment gyro (CMG). To overcome the deficiency of being trapped in the momentum saturation singularities, a new steering logic based on a mixed weighted two-norm and least squares optimization solution is presented. To reduce the torque output pressure of CMG system, a switching logic is designed for the hybrid actuators, and the cold air thruster system is proposed for the requirements of large torque to reduce the probability of singularity and CMG is selected for high-precision smooth. To obtain fast and high-precision control effect, ADRC is presented to control the three-axis air bearing table. The results show that the system can reach stabilization rapidly, the error and the attitude stability can reach a good level, effectively protecting the single gimbal control moment gyro (SGCMG) system from singular state, making full use of the system's capabilities, and verifying the validity of the hybrid actuators switching logic.
KW - Auto Disturbance Rejection Control
KW - Hybrid Actuators
KW - Single Gimbal Control Moment Gyro
KW - Three Axis Air Bearing Table
UR - https://www.scopus.com/pages/publications/85175523793
U2 - 10.23919/CCC58697.2023.10240756
DO - 10.23919/CCC58697.2023.10240756
M3 - 会议稿件
AN - SCOPUS:85175523793
T3 - Chinese Control Conference, CCC
SP - 7087
EP - 7092
BT - 2023 42nd Chinese Control Conference, CCC 2023
PB - IEEE Computer Society
T2 - 42nd Chinese Control Conference, CCC 2023
Y2 - 24 July 2023 through 26 July 2023
ER -