Adaptive control augmentation of a missile

Date

2010-01-01

Author

Kutluay, Kadriye Tiryaki
Yavrucuk, İlkay

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Adaptive control augmentation can be used for the controller design of air vehicles, eliminating the need for a detailed design process and accurate model data. This paper presents the application of the L1 adaptive control augmentation system to a baseline autopilot of a missile, which is designed with dynamic model inversion at a single flight condition. The output redefinition approach is used in the inversion process of the non-minimum phase transfer functions. The resulting controllers are examined through high fidelity, nonlinear, 6 D.o.F. simulations. © 2010 IFAC.

Subject Keywords

Adaptive augmentation, Adaptive control, Dynamic inversion, Output redefinition

URI

https://www.scopus.com/inward/record.uri?partnerID=HzOxMe3b&scp=84901910781&origin=inward
https://hdl.handle.net/11511/107176

DOI

https://doi.org/10.3182/20100826-3-tr-4015.00017

Conference Name

10th IFAC International Workshop on Adaptation and Learning in Control and Signal Processing, ALCOSP 2010

Collections

Department of Aerospace Engineering, Conference / Seminar

Citation Formats

K. T. Kutluay and İ. Yavrucuk, “Adaptive control augmentation of a missile,” Antalya, Türkiye, 2010, vol. 1, Accessed: 00, 2023. [Online]. Available: https://www.scopus.com/inward/record.uri?partnerID=HzOxMe3b&scp=84901910781&origin=inward.