Robust attitude controller for uncertain hexarotor micro aerial vehicles (MAVs)
This paper proposes a practical robust attitude controller for uncertain hexarotor micro aerial vehicles (MAVs). The proposed robust controller consists of a nominal linear time-invariant controller and a robust compensator for pitch, roll, and yaw subsystems. The nominal controller is an inner-oute...
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Main Authors: | , , , , |
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Format: | Article |
Published: |
Institute of Electrical and Electronics Engineers Inc.
2014
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Subjects: | |
Online Access: | http://eprints.utm.my/id/eprint/62493/ http://dx.doi.org/10.1109/IROS.2014.6943241 |
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