Nonsingular terminal sliding mode control technique for attitude tracking problem of a small satellite with combined energy and attitude control system (CEACS)
Authors:
- Samira EshghiSESamira Eshghi
- Renuganth VaratharajooRVRenuganth Varatharajoo
- 1 May 2018
- journal article
- research article
- Published by Elsevier in Aerospace Science and Technology
- Vol. 76, 14-26
Abstract
No abstract availableKeywords
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