On stability of a rotating spacecraft partially filled with liquid: The case of a single cavity

Details On stability of a rotating spacecraft partially filled with liquid: The case of a single cavity On stability of a rotating spacecraft partially filled with liquid: The case of a single cavity

May 2006

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2006cosre..44..226m&link_type=abstract

Cosmic Research, Volume 44, Issue 3, pp.226-235

Mathematics

45.20.Dc

Scientific paper

The problem of stability of a rotating spacecraft with a cavity partially filled with liquid to a small depth is considered with regard to the distinction in angular velocities of spacecraft and liquid rotation and their variability (the modes of the spacecraft’s stationary rotation, spin-up, and rotation deceleration). The regions of stability (in space of the characteristic parameters of an object) are found, and mathematical simulating of the disturbed motion is carried out.

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