Stability and Stabilization of Relative Equilibria of a Dumbbell Body in Central Gravity

A dumbbell-shaped rigid body can be used to represent certain large spacecraft or asteroids with bimodal mass distributions. Such a dumbbell body is modeled here as two identical mass particles connected by a rigid, massless link. Equations of motion for the five degrees of freedom of the dumbbell body in a central gravitational field are obtained. The equations of motion characterize three orbit degrees of freedom, two attitude degrees of freedom, and the coupling between them. The system has a continuous symmetry due to a cyclic variable associated with the angle of right ascension of the dumbbell body. Reduction with respect to this symmetry gives a reduced system with four degrees of freedom. Relative equilibria, corresponding to Graduate student, Department of Aerospace Engineering. Post-doctoral scholar, Department of Aerospace Engineering. Professor, Department of Aerospace Engineering, Fellow AIAA. This research has been supported in part by NSF under grant ECS-0140053. Professor, Department of Mathematics. This research has been supported in part by NSF under grants DMS-0103895 and DMS-0305837. 1 circular orbits, are obtained from these reduced equations of motion; stability of these relative equilibria is assessed. It is shown that unstable relative equilibria can be stabilized by suitable attitude feedback control of the dumbbell.