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- W2132176463 abstract "Launch vehicle volume and payload geometry often make advantageous a spacecraft design based on spin stabilization about a minor principal axis, at least for a portion of the spacecraft's lifetime. Frequently a reaction wheel, mounted transverse to the desired spin axis, is used to provide the necessary spin stabilization (or the equivalent active nutation damping on a major axis spinner). The control law for the reaction wheel is typically designed using full state feedback applied to the linearized equations of motion of the system. A new stabilizing reaction wheel control law is developed here, using a Lyapunov approach applied to the full non-linear equations of motion of the system. The reaction wheel dynamics are included in the system model. The new approach has an important advantage over the classical approach in that it provides control laws that are globally stable, i.e. it provides flat spin recovery for minor axis spinners. In the presence of input saturation the Lyapunov approach provides a rigorous description of a guaranteed region of convergence, which a linearized design cannot." @default.
- W2132176463 created "2016-06-24" @default.
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- W2132176463 date "2000-08-14" @default.
- W2132176463 modified "2023-09-27" @default.
- W2132176463 title "A Lyapunov design approach to nutation damping with a reaction wheel" @default.
- W2132176463 cites W2008406083 @default.
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- W2132176463 doi "https://doi.org/10.2514/6.2000-4047" @default.
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