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- W2323024148 abstract "Launch vehicle volume and payload geometry can often guide spacecraft design toward spin stabilization about a minor principal axis. But this requires full time control throughout the satellite’s mission life. For smaller satellites, magnetic control provides a simple and inexpensive method which requires no expendables and therefore does not limit the lifetime of the satellite. Currently, two magnetic nutation damping laws have been used in such applications. Both laws are based on heuristic derivations. A new magnetic nutation damping law is developed here, using a Lyapunov approach. This new law is equivalent to the previously available laws when the vehicles are axisymmetric; however, in the case of asymmetric vehicles, the Lyapunov-based law is superior in terms of nutation damping time. The Lyapunov development provides rigorous justification for the two existing magnetic nutation damping laws when applied to symmetric satellites. The new law also guarantees global convergence, within certain restrictions, thus providing for autonomous flat spin recovery of minor-axis spinning satellites." @default.
- W2323024148 created "2016-06-24" @default.
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- W2323024148 date "1999-08-09" @default.
- W2323024148 modified "2023-09-27" @default.
- W2323024148 title "A Lyapunov design approach to magnetic nutation damping" @default.
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- W2323024148 doi "https://doi.org/10.2514/6.1999-3971" @default.
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