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Pulse-width Control of a Flexible Spacecraft

Sergey Somov
Problems of nonlinear modeling, dynamic analysis and simulation of spatial motion by a spacecraft with flexible weak damping structure, are considered.
The obtained results on a multi-rate filtering measurements and a width-pulse modulation of the jet engine thrust control for the communication satellite with large-scale solar array panels at modes of initial damping and guidance on the Sun and on the Earth, are represented.
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