Robust attitude control design for a low-cost hexarotor micro aerial vehicle
This article proposes a new practical robust attitude state feedback controller of a low-cost hexarotor micro aerial vehicle under the effects of noise in angular velocity measurements and multiple uncertainties (called the equivalent disturbance), which consist of external time-varying wind disturb...
| Main Authors: | , , , , |
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| Format: | Article |
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SAGE Publications Ltd
2016
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