Attitude stabilization of a rigid spacecraft using two control torques: A nonlinear control approach based on the spacecraft attitude dynamics

@article{Krishnan1994AttitudeSO,
  title={Attitude stabilization of a rigid spacecraft using two control torques: A nonlinear control approach based on the spacecraft attitude dynamics},
  author={H. Krishnan and M. Reyhanoglu and N. McClamroch},
  journal={Autom.},
  year={1994},
  volume={30},
  pages={1023-1027}
}
  • H. Krishnan, M. Reyhanoglu, N. McClamroch
  • Published 1994
  • Mathematics, Computer Science
  • Autom.
  • The attitude stabilization problem of a rigid spacecraft using control torques supplied by gas jet actuators about only two of its principal axes is considered. If the uncontrolled principal axis of the spacecraft is not an axis of symmetry, then the complete spacecraft dynamics are small time locally controllable. However, the spacecraft cannot be asymptotically stabilized to any equilibrium attitude using time-invariant continuous feedback. A discontinuous stabi- lizing feedback control… CONTINUE READING
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