H. Bang et al., LYAPUNOV OPTIMAL-CONTROL LAWS FOR FLEXIBLE STRUCTURE MANEUVER AND VIBRATION CONTROL, The Journal of the astronautical sciences, 41(1), 1993, pp. 91-118
An approach is presented for optimization of Lyapunov stable control l
aws for maneuvering of a flexible structure. The main idea is to estab
lish a stabilizing control law using a Lyapunov approach and introduce
some optimality condition for a particular control objective, and the
n optimize over the stable region of the free parameters in the contro
l law. Our approach for designing the optimal control law consists of
two stages. The first stage is to find a stabilizing form for the cont
rol law as a function of design parameters which are usually feedback
gains. In the second stage, the control law is reshaped with the desig
n parameters to satisfy an optimality criteria. Two kinds of control s
chemes, constant gain feedback and tracking type control laws, are dis
cussed to establish different perspectives on the optimization. The op
timization scheme used in this work is a sequential nonlinear programm
ing algorithm which uses a homotopy method to sweep through a sequence
of minimum norm design parameter changes. Our results show how our co
ntrolled performance is improved by optimizing the parameters appearin
g in the reference trajectory as well as the associated tracking feedb
ack control law.