First integrals of motion in the dynamics of tethered satellites

Details First integrals of motion in the dynamics of tethered satellites First integrals of motion in the dynamics of tethered satellites

Sep 1986

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1986jansc..34..331r&link_type=abstract

Journal of the Astronautical Sciences (ISSN 0021-9142), vol. 34, July-Sept. 1986, p. 331-339.

Astronomy and Astrophysics

Astronomy

Equations Of Motion, Libration, Space Shuttle Payloads, Tethered Satellites, Dynamic Stability, Integrals, Systems Stability

Scientific paper

First integrals of motion in the planar librational deployment/retrieval dynamics of Shuttle-Tethered-Subsatellite systems are derived using Noether's theorem. The first integrals are useful in understanding the librational dynamics described by a nonautonomous equation of motion. The first integrals are used to investigate the stability of the system by Liapunov's second method.

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