TY - GEN
T1 - Analysis of Characteristics of Rigid Universal Joint of Gyrowheel
AU - Chen, Shuo
AU - Zhao, Hui
AU - Huo, Xin
AU - Yao, Yu
N1 - Publisher Copyright:
© 2018 IEEE.
PY - 2018/8
Y1 - 2018/8
N2 - As a new type of inertial actuator, the gyrowheel can perform actuator and sensor applied for micro-spacecraft. Due to the special support mechanical structure of gyrowheel rotor, the rotation speed of the rotor in the tilting would produce twice-spin frequency flutter, which affects the service life of system. In this paper, according to the rigid universal joint of the prototype, the mathematical model of speed transfer is established and the torque analysis of universal joint is carried out at the same time. The simulation results verified the effects of the joint on the gyrowheel.
AB - As a new type of inertial actuator, the gyrowheel can perform actuator and sensor applied for micro-spacecraft. Due to the special support mechanical structure of gyrowheel rotor, the rotation speed of the rotor in the tilting would produce twice-spin frequency flutter, which affects the service life of system. In this paper, according to the rigid universal joint of the prototype, the mathematical model of speed transfer is established and the torque analysis of universal joint is carried out at the same time. The simulation results verified the effects of the joint on the gyrowheel.
UR - https://www.scopus.com/pages/publications/85082492142
U2 - 10.1109/GNCC42960.2018.9019135
DO - 10.1109/GNCC42960.2018.9019135
M3 - 会议稿件
AN - SCOPUS:85082492142
T3 - 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018
BT - 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018
Y2 - 10 August 2018 through 12 August 2018
ER -