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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Main Authors: | Derawi, D., Salim, N. D., Zamzuri, H., Abdul Rahman, M. A., Nonami, K. |
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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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