Design of Non-Linear Dynamic Inversion UAV with QFT

Jie Li; Jie Zhang; Zhi Hui Xu

doi:10.4028/www.scientific.net/AMR.466-467.676

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 466-467Design of Non-Linear Dynamic Inversion UAV with...

Design of Non-Linear Dynamic Inversion UAV with QFT

Abstract:

Flight control system of UAV (Unmanned Aerial Vehicle) has limitations with non-linear dynamic inversion method. This paper introduces QFT based on non-linear dynamic inversion method, for avoiding model errors during existing non-linear function offset, QFT theory is presented firstly, then UAV model is established using non-linear dynamic inversion method, definituding the range of errors and system performance requirements, flight control system of UAV is designed with QFT, the simulating curves show that system has robustness stability.

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Periodical:

Advanced Materials Research (Volumes 466-467)

Pages:

676-679

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.466-467.676

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Online since:

February 2012

Authors:

Jie Li, Jie Zhang, Zhi Hui Xu

Keywords:

Non-Linear Dynamic Inversion, Quantitative Feedback Theory (QFT), Robust, Unmanned Aerial Vehicle (UAV)

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References

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