Abstract
The objective of this chapter is to develop a unified actuator nonlinearity compensation scheme for an aircraft augmented with SJs operating at a wide range of conditions, including both low and high AoA. The motivation for such a design is the intrinsically complicated nonlinear characteristic of a SJ when used for an aircraft operating in a wide range of AoA.
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References
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Deb, D., Tao, G., Burkholder, J., Smith, D.: Adaptive synthetic jet actuator compensation for a nonlinear tailless aircraft model at low angles of attack. In: 2006 American Control Conference (2006). https://doi.org/10.1109/acc.2006.1655376
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Deb, D., Burkholder, J., Tao, G. (2022). Adaptive Synthetic Jet Actuation for Aircraft Control. In: Adaptive Compensation of Nonlinear Actuators for Flight Control Applications. Studies in Systems, Decision and Control, vol 386. Springer, Singapore. https://doi.org/10.1007/978-981-16-4161-9_7
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DOI: https://doi.org/10.1007/978-981-16-4161-9_7
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