The planar motion of a rotating space station composed of a manned compartment and a counterweight linked by a long flexible cable is analyzed. It is assumed that initially the system is spinning in the orbital plane. The effects of cable elasticity and vibrational motion are included in the derivation of equations, which reveal that the orbital, rotational, and elastic degrees of freedom are coupled through the gravitational gradient terms. The re- sponses of the coupled nonlinear differential equations to the influence of gravitational gradi- ents are solved by the fourth-order Runge-Kutta numerical integration method. Viscous damping is included in the investigation and found to be effective to the gravitational excita- tion. From the results of the analysis, the feasibility of the configuration is evaluated, and the critical problem areas are discussed. Nomenclature a = sublength of cable d, = position vector from center of mass to a point on cable EA = extensional rigidity Gri, G'>, dGc — gravity forces on mi, m2, and elementary podrjo of cable members, cables, or chains are of considerable interest as structural elements for connecting the compartments or counterweights to form a space station. However, the exact dynamic behavior of a cable-linked configuration is difficult to predict. The deployment, spin-up, artificial gravity, docking capacity, control system, and wobble damping are all formidable problems of a cable-linked configuration. An- other critical question to be answered is whether the cable- connected system, oscillating under the influence of gravity gradient and other perturbing forces, is a stable configuration. Published information concerning dynamic problems of a cable-connected space station is limited. A majority of the authors confined their treatment of the libration of the orbit- ing vehicle to the assumption of small oscillation, and they neglected perturbations from the orbital elements.14 Past experience in the analysis of orbiting satellites indicated that, for a configuration like the cable-connected space sta- tion, the rotational and vibrational motion cannot be treated independently from orbital motion without violating the laws of conservation of energy and conservation of angular momentum.5 In this paper, the planar motion of a rotating space station composed of a manned compartment and a counterweight linked by a long flexible cable is analyzed. This space sta- tion is assumed to be in orbit around a spherical earth with an inverse-squar e-law gravitational field and to be spinning in its orbital plane. (The spin-up phase is not included in the analysis.) The stability and control characteristics may be significantly influenced by the distortions of the cable under transient loading conditions. The effects of cable elasticity and vibrational motion are included in the formu- lation. The time dependence of the elastic motion is based upon the deformation of the cable expressed in terms of its normal modes of free vibration. The equations of planar motion in the earth-fixed coordi- nates are derived from the total kinetic energy of the system, the strain energy of the cable, and the generalized force re- sulting from the work done by the gravitational gradient over the extended body. The resulting equations reveal that the orbital, rotational, and elastic degrees of freedom
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