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

Abstract

-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… (More)
DOI: 10.1016/0005-1098(94)90196-1

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@article{Krishnan1994AttitudeSO, title={Attitude stabilization of a rigid spacecraft using two control torques: A nonlinear control approach based on the spacecraft attitude dynamics}, author={Hariharan Krishnan and Mahmut Reyhanoglu and N. Harris McClamroch}, journal={Automatica}, year={1994}, volume={30}, pages={1023-1027} }