Dynamic Inversion Based Control of a Missile with L1 Adaptive Control Augmentation

Date

2010-09-10

Author

Kutluay, Kadriye Tiryaki
Yavrucuk, İlkay

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This work is licensed under a Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.

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Dynamic model inversion is a popular method for flight controllers of air vehicles reducing the need for gain scheduling. However, imperfect model inversion, and non-accurate aerodynamic data may cause degradation of performance, and may lead to un-stability of the controller. The novel L1 adaptive control augmentation system offers an adaptive element to augment the control signal to account for matched and un-matched system uncertainties. In this paper, dynamic inversion controllers designed for the control of a missile are augmented with L1 adaptive controllers. The resulting controllers are examined through high fidelity, nonlinear, 6 D.o.F. simulations.

Subject Keywords

Aerodynamics, Acceleration, Missiles, Nonlinear dynamical systems, Adaptive control, Adaptation model , Uncertainty

URI

https://hdl.handle.net/11511/41736

DOI

https://doi.org/10.1109/isic.2010.5612892

Collections

Department of Aerospace Engineering, Conference / Seminar

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Citation Formats

K. T. Kutluay and İ. Yavrucuk, “Dynamic Inversion Based Control of a Missile with L1 Adaptive Control Augmentation,” 2010, Accessed: 00, 2020. [Online]. Available: https://hdl.handle.net/11511/41736.