This paper introduces a procedure for a dynamic analysis to study the
motion trajectory of space robots using Kane's equations and Huston's
method. The space robot is considered as a multibody system consisting
of manipulators and the host spacecraft. Nonholonomic constraints on
the system are handled by using Lagrange multipliers and orthogonal co
mplement matrices while the redundancy is managed by using Hamilton's
law. Simulation results show that this procedure can efficiently be us
ed to solve space robot dynamics problems with redundant and nonholono
mic constraints. (C) 1997 Elsevier Science Ltd.