TY - JOUR
T1 - A static balancing mechanism with continuously variable payload capacity for space docking simulation
AU - Xue, Yuan
AU - Liu, Shiwei
AU - Wang, Zhihai
AU - Tao, Siyuan
N1 - Publisher Copyright:
© IMechE 2023.
PY - 2023/8
Y1 - 2023/8
N2 - In this paper, a novel static balancing mechanism is presented to realize gravity compensation in the application of the space docking simulation. By optimizing the relative positions of the compensation pulley block and suspension pulley block, the proposed gravity balancing device achieves static balance in geometry and hence is applicable to continuous variable payload environments. The static balancing mechanism is developed firstly, and its design philosophy is described in detail. By adopting the genetic algorithm (GA) and steepest descent method (SDM) simultaneously, the optimal structural configuration with small trajectory fluctuation in the direction of gravity is obtained. Furthermore, the effect of structural parameters on gravity compensation performance is evaluated. Experimental results and error analysis demonstrate the gravity balancing capability, which indicates the rationality and effectiveness of the proposed device in the space docking condition.
AB - In this paper, a novel static balancing mechanism is presented to realize gravity compensation in the application of the space docking simulation. By optimizing the relative positions of the compensation pulley block and suspension pulley block, the proposed gravity balancing device achieves static balance in geometry and hence is applicable to continuous variable payload environments. The static balancing mechanism is developed firstly, and its design philosophy is described in detail. By adopting the genetic algorithm (GA) and steepest descent method (SDM) simultaneously, the optimal structural configuration with small trajectory fluctuation in the direction of gravity is obtained. Furthermore, the effect of structural parameters on gravity compensation performance is evaluated. Experimental results and error analysis demonstrate the gravity balancing capability, which indicates the rationality and effectiveness of the proposed device in the space docking condition.
KW - Space docking simulator
KW - combined pulley block
KW - continuous variable payload
KW - error analysis
KW - gravity compensation mechanism
UR - https://www.scopus.com/pages/publications/85146555003
U2 - 10.1177/09544062221148418
DO - 10.1177/09544062221148418
M3 - 文章
AN - SCOPUS:85146555003
SN - 0954-4062
VL - 237
SP - 3459
EP - 3471
JO - Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science
JF - Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science
IS - 15
ER -