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Dynamics and Control for Large Angle Rapid Slew Maneuvering of a Flexible Multi-Body Spacecraft
Author(s): 
Pages: 57-62+69
Year: Issue:  4
Journal: Aerospace Control

Keyword:  Flexible spacecraftAttituteAttitute control;
Abstract: This paper is concerned wish the dynamics and control for planar, large anglerapid slew maneuvering of a flexible multi - body spacecraft, consisting of a rigid centralbody, a flexible beam and a rigid tip mass. Nonlinear infinite dimensional model of the sys-tem is derived by employing the Hamilton’s principle. By using the measurements of the atti-tude angle of the rigid central body and its angular rate only, a kind of linear feedback con-trol law is presented. It is shown that implementation of the control algorithm results inasymptotic stability of the closed - loop system .
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