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- JAFARI Hamidreza
- Department of Aerospace Engineering, K. N. Toosi University of Technology
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- ZAREH Mehran
- Department of Aerospace Engineering, K. N. Toosi University of Technology
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- ROSHANIAN Jafar
- Department of Aerospace Engineering, K. N. Toosi University of Technology
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- NIKKHAH Amirali
- Department of Aerospace Engineering, K. N. Toosi University of Technology
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抄録
The optimal guidance law of an autonomous four-rotor helicopter, called the Quadrotor, using linear quadratic regulators (LQR) is presented in this paper. The dynamic equations of the Quadrotor are considered nonlinear so to find an LQR controller, it is necessary that these equations be linearized in different operation points. Due to importance of energy consumption in Quadrotors, minimum energy is selected as the optimal criteria.
収録刊行物
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- TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 53 (179), 32-39, 2010
一般社団法人 日本航空宇宙学会
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詳細情報 詳細情報について
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- CRID
- 1390001204079615232
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- NII論文ID
- 10026520859
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- NII書誌ID
- AA0086707X
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- ISSN
- 21894205
- 05493811
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- NDL書誌ID
- 10673029
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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