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  L1-based Model Following Control of an Identified Helicopter Model in Hover

Picardi, G., Geluardi, S., Olivari, M., & Bülthoff, H. (2016). L1-based Model Following Control of an Identified Helicopter Model in Hover. In Leveraging Emerging Technologies for Future Capabilities (pp. 1770-1777). Red Hook, NY, USA: Curran.

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アイテムのパーマリンク: https://hdl.handle.net/21.11116/0000-0000-7A9C-8 版のパーマリンク: https://hdl.handle.net/21.11116/0000-0000-7A9D-7
資料種別: 会議論文

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 作成者:
Picardi, G1, 著者           
Geluardi, S1, 2, 3, 著者           
Olivari, M1, 2, 3, 4, 著者           
Bülthoff, HH1, 2, 3, 著者           
所属:
1Department Human Perception, Cognition and Action, Max Planck Institute for Biological Cybernetics, Max Planck Society, ou_1497797              
2Project group: Cybernetics Approach to Perception & Action, Max Planck Institute for Biological Cybernetics, Max Planck Society, ou_2528701              
3Max Planck Institute for Biological Cybernetics, Max Planck Society, ou_1497794              
4Project group: Motion Perception & Simulation, Max Planck Institute for Biological Cybernetics, Max Planck Society, ou_2528705              

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 要旨: The aim of this study is to augment the uncertain dynamics of the helicopter in order to resemble the dynamics of a new kind of vehicle, the so called Personal Aerial Vehicle. To achieve this goal a two step procedure is proposed. First, the helicopter model dynamics is augmented with a PID-based dynamic controller. Such controller implements a model following on the nominal helicopter model without uncertainties. Then, an L1 adaptive controller is designed to restore the nominal responses of the augmented helicopter when variations in the identified parameters are considered. The performance of the adaptive controller is evaluated via Montecarlo simulations. The results show that the application of the adaptive controller to the augmented helicopter dynamics can significantly reduce the effects of uncertainty due to the identification of the helicopter model. For implementation reasons the adaptive controller was applied to a subset of the outputs of the system. However, the under actuation typical of helicopters makes the tracking of the nominal responses good also on the not directly adapted outputs.

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 日付: 2016-05
 出版の状態: 出版
 ページ: -
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 識別子(DOI, ISBNなど): BibTex参照ID: PicardiGOB2016
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関連イベント

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イベント名: 72nd American Helicopter Society International Annual Forum (AHS 2016)
開催地: West Palm Beach, FL, USA
開始日・終了日: -

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出版物名: Leveraging Emerging Technologies for Future Capabilities
種別: 会議論文集
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出版社, 出版地: Red Hook, NY, USA : Curran
ページ: - 巻号: - 通巻号: - 開始・終了ページ: 1770 - 1777 識別子(ISBN, ISSN, DOIなど): ISBN: 978-1-5108-2506-2