Authors

Houria Siguerdidjane

Abstract

This paper is dealing with the control of a rigid spacecraft. The nonlinear feedback controls, derived by using the approaches that have been recently developed, based on the port controlled hamiltonian (PCH) structure, are compared to the one derived by the methods based on the eigenstructure proposed by the author in previous work. The aim is to emphasize that, using the second approach appears as a particular case than using the first approach. Moreover, the results have been applied to derive the control laws of a launcher in the phase outside the atmosphere. It may be interesting to observe that the coefficients of the damping matrix, involved in PCH approach, have not the same effect on the system sensitivity. This paper somehow extends the related one presented by the author at the IFAC symposium in aerospace control.

Keywords

nonlinear feedback control, port controlled hamiltonian structure, rigid body

Citation

  • Journal: IFAC Proceedings Volumes
  • Year: 2002
  • Volume: 35
  • Issue: 1
  • Pages: 133–138
  • Publisher: Elsevier BV
  • DOI: 10.3182/20020721-6-es-1901.01247
  • Note: 15th IFAC World Congress

BibTeX

@article{Siguerdidjane_2002,
  title={{SOME REMARKS ON NONLINEAR FEEDBACK CONTROL OF A RIGID SPACECRAFT}},
  volume={35},
  ISSN={1474-6670},
  DOI={10.3182/20020721-6-es-1901.01247},
  number={1},
  journal={IFAC Proceedings Volumes},
  publisher={Elsevier BV},
  author={Siguerdidjane, Houria},
  year={2002},
  pages={133--138}
}

Download the bib file

References

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