An Optimal Guidance Law Applied to Quadrotor Using LQR Method
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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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Abstract
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.
Journal
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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
THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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Keywords
Details 詳細情報について
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- CRID
- 1390001204079615232
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- NII Article ID
- 10026520859
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- NII Book ID
- AA0086707X
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- ISSN
- 21894205
- 05493811
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- NDL BIB ID
- 10673029
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- Text Lang
- en
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- Data Source
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- JaLC
- NDL
- Crossref
- CiNii Articles
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- Abstract License Flag
- Disallowed