Attitude stabilization of a rigid spacecraft using two control torques: A nonlinear control approach based on the spacecraft attitude dynamics
- 30 June 1994
- journal article
- research article
- Published by Elsevier BV in Automatica
- Vol. 30 (6), 1023-1027
- https://doi.org/10.1016/0005-1098(94)90196-1
Abstract
No abstract availableKeywords
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- On the Synthesis of a Stabilizing Feedback Control via Lie Algebraic MethodsSIAM Journal on Control and Optimization, 1980