On the Attitude Stabilization of a Rigid Spacecraft Using Two Control Torques

@article{Krishnan1992OnTA,
  title={On the Attitude Stabilization of a Rigid Spacecraft Using Two Control Torques},
  author={Hariharan Krishnan and Harris N. McClamroch and Mahmut Reyhanoglu},
  journal={1992 American Control Conference},
  year={1992},
  pages={1990-1995}
}
The attitude stabilization problem of a rigid spacecraft using only two control torques is considered. The control torques are assumed to be generated by either gas jet actuators or momentum wheel actuators. In particular, we focus on the development of a control strategy for the following two problems which have not been considered elsewhere: the attitude stabilization of an axially symmetric spacecraft using control torques supplied by two pairs of gas jet actuators about axes spanning a two… CONTINUE READING
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