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...

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Bibliographic Details
Main Authors: Derawi, D., Salim, N. D., Zamzuri, H., Abdul Rahman, M. A., Nonami, K.
Format: Article
Published: SAGE Publications Ltd 2016
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Online Access:http://eprints.utm.my/id/eprint/71608/
https://www.scopus.com/inward/record.uri?eid=2-s2.0-84976438435&doi=10.1177%2f0142331215625768&partnerID=40&md5=de9b6d1fbbd49652b6160e7ce9e9f15d
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