Electronic Resource
Springer
Journal of optimization theory and applications
50 (1986), S. 83-108
ISSN:
1573-2878
Keywords:
Flexible spacecraft
;
dynamic modelling
;
coupled systems of ordinary and partial differential equations
;
system stabilization
;
Lyapunov's functionals
;
feedback control
Source:
Springer Online Journal Archives 1860-2000
Topics:
Mathematics
Notes:
Abstract We consider the problem of rigorous modelling of flexible spacecraft and their stabilization. It is shown that the dynamics of the flexible spacecraft can be described by a coupled system of ordinary differential equations and partial differential equations (hybrid system). Lyapunov's approach is used to prove the stabilizability of the system. Simple feedback controls are suggested for stabilization of flexible spacecraft.
Type of Medium:
Electronic Resource
URL:
http://dx.doi.org/10.1007/BF00938479
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