Fuzzy logic-based adaptive control system for in-orbit assembly of large space structures

Design of a fuzzy adaptive algorithm to control orientation of a large space structure during the progress of in-orbit assembly was considered. For the discretely evolving structure, a matrix description of the set of modal-physical models was given. Introduced were the functions of influence of the basic control on the dynamics of the autonomous models of isolated flexible modes that underlie the fuzzy characteristics of the orientation system. A methodology of designing a fuzzy logic-based adaptive algorithm for stabilization of a transformable flexible multifrequency space object was proposed. The results of simulating the proposed adaptive orientation system were presented.

Presented by the member of Editorial Board: A. P. Kurdyukov