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Hybrid and supervisory control of a rigid body

Abstract : We present several switching controllers for the attitude stabilization of a spacecraft. The control laws are reminiscent of classic controllers for robot manipulators, adapted to the topology of the quaternion space, in which the model of the spacecraft is expressed. A switching law is incorporated to deal with multiplicity of equilibria, inherent to the rigid-body model. Another controller based on a hysteresis supervisor is presented. This may be seen as a switching controller which commutes between two switching controllers. Detailed simulation results are also included where the emphasis is put into an adequate tunning; in particular, it is showed that with an appropriate switching law one may significantly decrease fuel consumption which directly translates into spacecraft lifespan.
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https://hal-supelec.archives-ouvertes.fr/hal-00521522
Contributor : Antonio Loria <>
Submitted on : Monday, September 27, 2010 - 5:31:02 PM
Last modification on : Wednesday, September 16, 2020 - 4:42:47 PM

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Rune Schlanbusch, Antonio Loria, P. J. Nicklasson. Hybrid and supervisory control of a rigid body. 49th. IEEE Conf. Decision Control, Dec 2010, Atlanta, United States. pp.528-533, ⟨10.1109/CDC.2010.5717827⟩. ⟨hal-00521522⟩

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