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- W4289883963 abstract "In order to solve the fast large-angle attitude maneuver and high-accuracy control problem for earth observation agile satellite flying mission, a control allocation strategy by combining control moment gyroscope (CMG) and flywheels is proposed. Based on the constrained optimization method, a control torques allocation method can be obtained by designing an optimization objective function related to CMG singularity index and energy-like rotation rate. By adjusting weight parameters properly, the flywheel rotation rate saturation and CMG singularity problems during the control process are solved. In addition, nondimensional conditions number and inner product singularity index for reliable computation of a gradient vector are also introduced to improve the control performance. Finally, effectiveness of the proposed strategy is demonstrated by numerical simulations." @default.
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- W4289883963 date "2022-01-01" @default.
- W4289883963 modified "2023-10-18" @default.
- W4289883963 title "A control allocation approach for hybrid actuators" @default.
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- W4289883963 doi "https://doi.org/10.1016/b978-0-323-95455-6.00008-1" @default.
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