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Adaptive Synthetic Jet Actuation for Aircraft Control

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Adaptive Compensation of Nonlinear Actuators for Flight Control Applications

Part of the book series: Studies in Systems, Decision and Control ((SSDC,volume 386))

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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

  1. Deb, D., Tao, G., Burkholder, J., Smith, D.: An adaptive inverse control scheme for a synthetic jet actuator model. In: Proceedings of the 2005, American Control Conference (2005). https://doi.org/10.1109/acc.2005.1470367

  2. 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

  3. Deb, D., Tao, G., Burkholder, J., Smith, D.: An adaptive inverse control scheme for synthetic jet actuator arrays. In: Infotech@Aerospace (2005). https://doi.org/10.2514/6.2005-7170

  4. Deb, D., Tao, G., Burkholder, J.: An adaptive inverse compensation scheme for signal-dependent actuator nonlinearities. In: 2007 46th IEEE Conference on Decision and Control (2007). https://doi.org/10.1109/cdc.2007.4434743

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Correspondence to Dipankar Deb .

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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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