Reduced-Order Observer Based Sliding Mode Control for a Quad-Rotor Helicopter
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- Akbar Reesa
- Department of Mechanical Engineering, Toyohashi University of Technology Department of Electrical Engineering, Politeknik Elektronika Negeri Surabaya
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- Sumantri Bambang
- Department of Mechanical Engineering, Toyohashi University of Technology Department of Electrical Engineering, Politeknik Elektronika Negeri Surabaya
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- Katayama Hitoshi
- Department of Electrical and Electronic Engineering, Shizuoka University
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- Sano Shigenori
- Department of Mechanical Engineering, Toyohashi University of Technology
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- Uchiyama Naoki
- Department of Mechanical Engineering, Toyohashi University of Technology
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<p>The reduced-order observer design we present estimates the velocity states of a quadrotor helicopter, or quadcopter, based on sampled measurements of position and attitude states. This observer is based on the forward-differentiation Euler model. The observer is robust enough against observation noise that the gain of a closed-loop controller is high enough to improve control performance. A sliding-mode controller stabilizes and implements quadcopter tracking control effectively, as is verified experimentally when compared to a conventional backward-difference method.</p>
収録刊行物
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- Journal of Robotics and Mechatronics
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Journal of Robotics and Mechatronics 28 (3), 304-313, 2016-06-20
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詳細情報 詳細情報について
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- CRID
- 1390282763127203712
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- NII論文ID
- 130007671068
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- NII書誌ID
- AA10809998
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- ISSN
- 18838049
- 09153942
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- NDL書誌ID
- 027568420
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- 本文言語コード
- en
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- データソース種別
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- JaLC
- NDL
- Crossref
- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可