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- W2516493419 abstract "Abstract When a stratospheric satellite travels by prevailing winds in the stratosphere, its cross-track displacement needs to be controlled to keep a constant latitude orbital flight. To design the orbit control system, a 6 degree-of-freedom (DOF) model of the satellite is established based on the second Lagrangian formulation, it is proven that the input/output feedback linearization theory cannot be directly implemented for the orbit control with this model, thus three subsystem models are deduced from the 6-DOF model to develop a sequential nonlinear control strategy. The control strategy includes an adaptive controller for the balloon-tether subsystem with uncertain balloon parameters, a PD controller based on feedback linearization for the tether-sail subsystem, and a sliding mode controller for the sail-rudder subsystem with uncertain sail parameters. Simulation studies demonstrate that the proposed control strategy is robust to uncertainties and satisfies high precision requirements for the orbit flight of the satellite." @default.
- W2516493419 created "2016-09-16" @default.
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- W2516493419 creator A5061657570 @default.
- W2516493419 date "2016-12-01" @default.
- W2516493419 modified "2023-10-05" @default.
- W2516493419 title "Orbit control of a stratospheric satellite with parameter uncertainties" @default.
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- W2516493419 doi "https://doi.org/10.1016/j.asr.2016.08.015" @default.
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