Physics
Scientific paper
Apr 2010
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2010cosre..48..194m&link_type=abstract
Cosmic Research, Volume 48, Issue 2, pp.194-204
Physics
Scientific paper
Dynamics of a satellite-stabilizer system is studied. It is supposed that there is a viscous friction in a hinge connecting two bodies, but there is no elasticity. The attitude motion in a plane of circular orbit is considered, and parameters are determined, at which natural oscillations near a stable equilibrium position in the orbital coordinate system are damped out most rapidly. The rate of transient processes is estimated by a value of the degree of stability of linearized equations of motion. The optimization of the degree of stability is sequentially performed in dimensionless damping coefficient (the first stage) and in inertial system parameters (the second stage). The result of the first stage is the partition of system parameter space into the regions, in each of which the maximum of the degree of stability is reached on a particular configuration of roots of the characteristic equation. It is shown at the second stage that the global maximum is reached at two points of parameter space, where one of system bodies degenerates into a plate, and the characteristic equation has four equal real roots.
Mirer S. A.
Prilepskiy I. V.
No associations
LandOfFree
Optimum parameters of a gravitational satellite-stabilizer system does not yet have a rating. At this time, there are no reviews or comments for this scientific paper.
If you have personal experience with Optimum parameters of a gravitational satellite-stabilizer system, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Optimum parameters of a gravitational satellite-stabilizer system will most certainly appreciate the feedback.
Profile ID: LFWR-SCP-O-1314054