In the station keeping phase, the in-plane pitch motion of a two body tethered satellite system, that is revolving around the Earth in a Keplerian circular orbit, is similar to the motion of a simple pendulum, i.e. the local vertical position is a center with small oscillations about it, and the local horizontal is a saddle point. However, if the three-dimensional coupled pitch and roll motions are considered, the dynamics of the system exhibit quasi-periodic and chaotic behavior. In order to study the control of the quasiperiodic and chaotic motions of a two-body tethered satellite system, which moves along a Keplerian circular orbit, this paper proposes to suppress the quasi-periodic and chaotic dynamics during deployment and retrieval, by applying a non-linear tension force along the connecting tether. A Lyapunov approach is used to design the non-linear tension for controlling tether deployment and retrieval. The goal of the control is to steer the sub-satellite from quasi-periodic and chaotic states to the local upward vertical position. The numerical simulations show that the non-linear tension control law performs well, reduces the quasi-periodic and chaotic oscillations, and the three-dimensional trajectories can be guided close to the local vertical direction.