TY - GEN
T1 - Dynamics of a rigid multibody system with loop constraints using only independent motion variables
AU - Jia, Yinghong
AU - Xu, Shijie
AU - Hu, Quan
PY - 2011
Y1 - 2011
N2 - This paper presents a reduced order dynamical formulation for a hinge-connected rigid multibody system with loop constrains in which only independent motion variables appear. A tree configuration system with a base body and branch chains is firstly acquired by cutting one of the loop bodies in half, and general equations of motion are formulated using a matrix version of Kane's equations where explicit expressions of the system mass matrix and nonlinear forces are presented. Then, with the constraint equations in terms of time derivatives of motion variables, reduced-order equations for the loop constrained system are formulated using a new form of Kane's equations for constrained system without introducing any multipliers such that the number of dimensions of the equations is equal to the number of degrees of freedom. Finally, a numerical simulation based on a space robot is carried out using both the formulation presented and the dynamic software ADAMS, and the results demonstrate the approach of this paper.
AB - This paper presents a reduced order dynamical formulation for a hinge-connected rigid multibody system with loop constrains in which only independent motion variables appear. A tree configuration system with a base body and branch chains is firstly acquired by cutting one of the loop bodies in half, and general equations of motion are formulated using a matrix version of Kane's equations where explicit expressions of the system mass matrix and nonlinear forces are presented. Then, with the constraint equations in terms of time derivatives of motion variables, reduced-order equations for the loop constrained system are formulated using a new form of Kane's equations for constrained system without introducing any multipliers such that the number of dimensions of the equations is equal to the number of degrees of freedom. Finally, a numerical simulation based on a space robot is carried out using both the formulation presented and the dynamic software ADAMS, and the results demonstrate the approach of this paper.
UR - http://www.scopus.com/inward/record.url?scp=84864102084&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:84864102084
SN - 9781618398055
T3 - 62nd International Astronautical Congress 2011, IAC 2011
SP - 5009
EP - 5020
BT - 62nd International Astronautical Congress 2011, IAC 2011
T2 - 62nd International Astronautical Congress 2011, IAC 2011
Y2 - 3 October 2011 through 7 October 2011
ER -