Stabilization of a spacecraft with asymmetric elastic design in geostationary orbit

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Approaches to the study of priority problems of long-term angular stabilization of information satellites and space robots with asymmetric elastic design in geostationary orbit are analyzed.

Spacecraft, asymmetric flexible design, geostationary orbit, stabilization

Короткий адрес: https://sciup.org/148314191

IDR: 148314191

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