An Aircraft Adaptive Control Architecture Based on Nominal Controller

Bo Zhang; Shu Shan Wang

doi:10.4028/www.scientific.net/AMR.490-495.105

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 490-495An Aircraft Adaptive Control Architecture Based on...

An Aircraft Adaptive Control Architecture Based on Nominal Controller

Abstract:

This paper presents adaptive control architecture for the safe flight of a transport aircraft under adverse operating conditions and uncertainties. This architecture combines a nominal controller based on an LQR with integral action, and an adaptive controller that accommodates for actuator saturation and disturbances. In this paper, we consider the control of the C-5 transport aircraft, which is similar to the Generic Transport Model. We delineate the underlying nonlinear dynamic model and introduce various upsets, damages, and failures by representing these various adverse conditions in the form of uncertainties.

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Periodical:

Advanced Materials Research (Volumes 490-495)

Pages:

105-109

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.490-495.105

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Online since:

March 2012

Authors:

Bo Zhang, Shu Shan Wang

Keywords:

Adaptive Control Architecture, Aircraft, Nominal Controller

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References

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