Adaptive Compensation Control of Synthetic Jet Actuator Arrays for Airfoil Virtual Shaping
In this paper, a new technology for control of next generation airplanes with virtual aerodynamic wing shaping using synthetic jet actuators is presented. The synthetic jets modify the local flow using a voltage driven vibrating diaphragm. The actuator array outputs are controlled by modulating the...
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| Veröffentlicht in: | Journal of aircraft 2007-03, Vol.44 (2), p.616-626 |
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| container_title | Journal of aircraft |
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| creator | Deb, Dipankar Tao, Gang Burkholder, Jason O Smith, Douglas R |
| description | In this paper, a new technology for control of next generation airplanes with virtual aerodynamic wing shaping using synthetic jet actuators is presented. The synthetic jets modify the local flow using a voltage driven vibrating diaphragm. The actuator array outputs are controlled by modulating the peak-to-peak amplitude of the input voltage. Nonlinear parameterized models of synthetic jet actuators whose parameters are chosen from a baseline model are presented. Adaptive inverse arrays are employed for canceling the effect of the jet nonlinearities. A state feedback control law is used for controlling aircraft dynamics. Parameter projection-based adaptive laws are used to ensure desired closed-loop stability and asymptotic tracking. An adaptive inverse scheme that is robust to modeling errors and parametric uncertainties of the synthetic jets is also presented. [PUBLICATION ABSTRACT] |
| doi_str_mv | 10.2514/1.24910 |
| format | Article |
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The synthetic jets modify the local flow using a voltage driven vibrating diaphragm. The actuator array outputs are controlled by modulating the peak-to-peak amplitude of the input voltage. Nonlinear parameterized models of synthetic jet actuators whose parameters are chosen from a baseline model are presented. Adaptive inverse arrays are employed for canceling the effect of the jet nonlinearities. A state feedback control law is used for controlling aircraft dynamics. Parameter projection-based adaptive laws are used to ensure desired closed-loop stability and asymptotic tracking. An adaptive inverse scheme that is robust to modeling errors and parametric uncertainties of the synthetic jets is also presented. 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| ispartof | Journal of aircraft, 2007-03, Vol.44 (2), p.616-626 |
| issn | 0021-8669 1533-3868 |
| language | eng |
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| source | Alma/SFX Local Collection |
| subjects | Aerodynamics Air transportation and traffic Aircraft Applied sciences Arrays Exact sciences and technology Feedback control systems Flow control Fluid dynamics Fundamental areas of phenomenology (including applications) Ground, air and sea transportation, marine construction Nonlinear programming Physics |
| title | Adaptive Compensation Control of Synthetic Jet Actuator Arrays for Airfoil Virtual Shaping |
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