Robust control of a morphing airfoil structure
This paper presents several robust control designs for a MIMO morphing airfoil concept. A linear aeroelastic model of the morphing wing is utilized to design an H/sub /spl infin// controller and a two degree of freedom H/sub /spl infin// loop shaping controller that track commanded lift and roll mom...
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| creator | Whitmer, C.E. Kelkar, A.G. |
| description | This paper presents several robust control designs for a MIMO morphing airfoil concept. A linear aeroelastic model of the morphing wing is utilized to design an H/sub /spl infin// controller and a two degree of freedom H/sub /spl infin// loop shaping controller that track commanded lift and roll moments. These methodologies are developed, along with the robustness conditions for input multiplicative, and real parametric uncertainty in /spl omega//sub n/ and /spl sigmav//sub n/. The robustness of each of these controllers is then evaluated using these conditions and the structured singular value (SSV). Comments and discussion on these control methodologies are then drawn presented. |
| doi_str_mv | 10.1109/ACC.2005.1470404 |
| format | Conference Proceeding |
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| ispartof | 2005 American Control Conference, 2005, p.2863-2868 vol. 4 |
| issn | 0743-1619 2378-5861 |
| language | eng |
| recordid | cdi_proquest_miscellaneous_29020093 |
| source | IEEE Electronic Library (IEL) Conference Proceedings |
| subjects | Actuators Aerodynamics Automotive components Equations Mathematical model Mechanical engineering Robust control Robust stability Shape control Uncertainty |
| title | Robust control of a morphing airfoil structure |
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