In this paper, we consider the planar motion of a free-flying robot equippe
d with the jet thrust mechanism. Based on the non-linear equations of motio
n of the free-flying robot, we calculate the optimal control such that the
fuel consumption is minimized and that the given terminal condition is sati
sfied at the end of motion. We use Sakawa-Shindo algorithm for calculating
the optimal control, which was derived on the basis of Pontryagin's maximum
principle. The computational results are satisfactory and show that the al
gorithm works well. Copyright (C) 1999 John Wiley & Sons, Ltd.