Abstract
Abstract This paper examines attitude tracking problem with unknown actuator dead-zone nonlinearity. A robust adaptive controller with parameter update laws is proposed and analyzed. A smooth inverse of the dead-zone is introduced to compensate for the effect of the dead-zone in controllers design with the adaptive control approach. The dead-zone parameters and the upper bound of the disturbance-like term are estimated by adaptive schemes. The stability of the resulting closed-loop systems is proved by application of Barbalat's Lemma. Numerical simulations are presented to show the effectiveness of the proposed attitude tracking approach.
| Original language | English |
|---|---|
| Article number | 3329 |
| Pages (from-to) | 196-202 |
| Number of pages | 7 |
| Journal | Aerospace Science and Technology |
| Volume | 45 |
| DOIs | |
| State | Published - 3 Jun 2015 |
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