| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 1715015 | Acta Astronautica | 2013 | 21 Pages |
Abstract
⺠Coupled translation and rotation error dynamics of a rigid spacecraft is modeled. ⺠A robust adaptive integrated control scheme is proposed. ⺠An auxiliary signal is introduced to handle control saturation. ⺠The uniformly ultimate bounded stability is guaranteed. ⺠Given the nominal case, the asymptotic stability is further ensured.
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Authors
Feng Zhang, Guangren Duan,