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The dynamics of a rotating tethered satellite system(TSS) in the vicinity of libration points are highly nonlinear and inherently unstable.In order to fulfll the station-keep control of the rotating TSS along halo orbits,a nonlinear output tracking control scheme based on the h–D technique is proposed.Compared with the popular time-variant linear quadratic regulator(LQR) controller,this approach overcomes some limitations such as on-line computations of the algebraic Riccati equation.Besides,the obtained nonlinear suboptimal controller is in a closed form and easy to implement.Numerical simulations show that the TTS trajectories track the periodic reference orbit with low energy consumption in the presence of both tether and initial injection errors.The axis of rotation can keep pointing to an inertial specifc object to fulfll an observation mission.In addition,the thrusts required by the controller are in an acceptable range and can be implemented through some low-thrust propulsion devices.
The dynamics of a rotating tethered satellite system (TSS) in the vicinity of libration points are highly nonlinear and inherently unstable. In order to fulfill the station-keep control of the rotating TSS along halo orbits, a nonlinear output tracking control scheme based on the h-D technique is proposed. Compared with the popular time-variant linear quadratic regulator (LQR) controller, this approach overcomes some limitations such as on-line computations of the algebraic Riccati equation. Besides, the resulting nonlinear suboptimal controller is in a closed form and easy to implement. Numerical simulations show that the TTS trajectories track the periodic reference orbit with low energy consumption in the presence of both tether and initial injection errors. The axis of rotation can keep pointing to an inertial specifc object to fulfll an observation mission .In addition, the thrusts required by the controller are in an acceptable range and can be implemented through some low-thrust propulsion devices.