Optimal stabilization of the steady motions of a spacecraft relative to its center of mass at a triangular libration point

Details Optimal stabilization of the steady motions of a spacecraft relative to its center of mass at a triangular libration point Optimal stabilization of the steady motions of a spacecraft relative to its center of mass at a triangular libration point

Nov 1981

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1981kosis..19..829b&link_type=abstract

Kosmicheskie Issledovaniia, vol. 19, Nov.-Dec. 1981, p. 829-834. In Russian.

Physics

Center Of Mass, Dynamic Stability, Libration, Spacecraft Motion, Three Body Problem, Canonical Forms, Equations Of Motion, Functionals, Optimization, Perturbation Theory

Scientific paper

The paper considers the problem of the optimal stabilization of the steady motion of a dynamically symmetric spacecraft relative to its center of mass on the basis of forces acting with respect to the cyclic coordinate and variations of the moments of inertia of the spacecraft. It is assumed that the center of mass of the spacecraft is located at the triangular libration point of the circular restricted three-body problem.

Affiliated with

Also associated with

No associations

Rating

Optimal stabilization of the steady motions of a spacecraft relative to its center of mass at a triangular libration point 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 Optimal stabilization of the steady motions of a spacecraft relative to its center of mass at a triangular libration point, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Optimal stabilization of the steady motions of a spacecraft relative to its center of mass at a triangular libration point will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFWR-SCP-O-744464