Future space systems will use teleoperated robotic systems mounted on
flexible bases such as the Shuttle Remote Manipulator System. Due to d
ynamic coupling, a major control issue associated with these systems i
s the effect of flexible base vibrations on the performance of the rob
ot. If uncompensated, flexible vibrations can lead to inertial trackin
g errors and an overall degradation in system performance. One way to
overcome this problem is to use kinematically redundant robots. Thus,
this article presents research results obtained from locally resolving
kinematic redundancies to reduce or damp flexible vibrations. Using a
planar, three-link rigid robot example, numerical simulations were pe
rformed to evaluate the feasibility of three vibration damping redunda
ncy control algorithms. Results showed that compared to a zero redunda
ncy baseline, the three controllers were able to reduce base vibration
by as much as 90% in addition to decreasing the required amount of jo
int torque. However, similar to locally optimizing joint torques, exce
ssive joint velocities often occurred. To improve stability, fixed wei
ght, multi-criteria optimizations were performed. (C) 1995 John Wiley
& Sons, Inc.