Authors

Houria Siguerdidjane, Hugo Rodriguez

Abstract

It is proposed the nonlinear feedback control of a rigid body angular momentum by using the nonlinear approaches that have been developed very recently and which are based on the port controlled hamiltonian structure. The aim of the present paper is to emphasize the fact that, the solutions may be readily derived by shaping the stored energy of the system. One has to look for simple expressions of the controller in the perspective of its implementation.

Keywords

Nonlinear Feedback control; rigid spacecraft; Port Controlled Hamiltonian Structure

Citation

  • Journal: IFAC Proceedings Volumes
  • Year: 2001
  • Volume: 34
  • Issue: 15
  • Pages: 147–152
  • Publisher: Elsevier BV
  • DOI: 10.1016/s1474-6670(17)40719-1
  • Note: 15th IFAC Symposium on Automatic Control in Aerospace, Bologna/Forlì, Italy, September 2-7, 2001

BibTeX

@article{Siguerdidjane_2001,
  title={{Regulation of Rigid Spacecraft Angular Momentum Using Port Controlled Hamiltonian Structure}},
  volume={34},
  ISSN={1474-6670},
  DOI={10.1016/s1474-6670(17)40719-1},
  number={15},
  journal={IFAC Proceedings Volumes},
  publisher={Elsevier BV},
  author={Siguerdidjane, Houria and Rodriguez, Hugo},
  year={2001},
  pages={147--152}
}

Download the bib file

References

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