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- W2333820175 abstract "This paper presents a novel stability analysis of the zero dynamics of nonlinear dynamic models of spacecraft with fuel slosh. Mathematical models based on a Lagrange formulation are used, with the pendulum analogy of a typical spacecraft with fuel slosh dynamics, to include the behavior of the liquid dynamics coupled to the spacecraft. With both analytical and numerical results, it is shown that in the presence of fuel sloshing, the zero dynamics of both single-input single-output and multi-input multi-output spacecraft models are not asymptotically stable or even unstable at their nominal equilibrium point. This study indicates that special design considerations are needed for nonlinear feedback motion control of spacecraft with fuel sloshing uncertainties, to handle the nonminimum phase characteristics of nonlinear spacecraft models, which are shown by the phase portraits of their zero dynamics. The development of suitable control designs for such nonlinear systems is currently under investigation." @default.
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- W2333820175 date "2008-06-15" @default.
- W2333820175 modified "2023-09-26" @default.
- W2333820175 title "Zero Dynamics Analysis for Spacecraft with Fuel Slosh" @default.
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- W2333820175 doi "https://doi.org/10.2514/6.2008-6455" @default.
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