Optimal control of flapping wing accounting for nonsteady effects
The optimization of flapping wing trajectory for the minimization energy consumed by the wing and associated with induced power losses is considered in this paper. An aircraft with such a wing is assumed to move in a horizontal direction at constant velocity. The flapping wing moves up and down at...
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| Format: | Article |
| Language: | English |
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Vilnius Gediminas Technical University
2010-03-01
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| Series: | Aviation |
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| Online Access: | https://www.tede.vgtu.lt/index.php/Aviation/article/view/5669 |