The paper focuses on indirect adaptive control of space robot manipula
tors when maneuvering payloads with imperfectly known mechanical param
eters. The objective is to estimate system mechanical parameters durin
g the maneuver itself. The system bodies are rigid, and are concatenat
ed by ideal, rotational joints. Existing adaptive control laws are inv
estigated in an application to a rotating. single-degree-of-freedom bo
dy. Even in this simple case, and more so in general multibody cases,
improvements in adaptive control laws are found to be needed. A new ad
aptive control law is developed which is applicable to general, rigid,
multibody systems. It is based on the reinterpretation of the system
dynamic equations as a measurement equation. The adaptive control law
is of the ''integrated'' type, i.e. the estimator part is used to esti
mate the integrated influence of the system mechanical parameters, rat
her than the parameters themselves. The controller part (the control l
aw proper) is of the ''certainty equivalence'' type. For the single-de
gree-of-freedom case, the system formal solution is presented. Then th
e parameter estimation process and the control law are separately anal
yzed to show that the control system output error is globally asymptot
ically stable, as well as the parameter error, provided the external c
ommand input satisfies a persistent excitation condition. In one numer
ical example it is shown how a two-armed, nine-degree-of-freedom space
robot can be controlled almost as if the mechanical parameters were p
erfectly known. Copyright (C) 1996 Elsevier Science Ltd