Trajectory tracking method for uav based on intelligent adaptive control and dynamic inversion

Juan Dai*, Yuanqing Xia

*Corresponding author for this work

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

This paper discusses the flight control strategy based on intelligent adaptive control and dynamic inversion. The primary use of the Optimal Control Modification (OCM) adaptive control is to add damping to the neural network controller weight update law so as to reduce high-frequency oscillations in the weights and to prevent parameter drift in the absence of persistent excitation. The OCM is applied to the inner loop control of an UAV during flight conditions to investigate its flight control augmentation capability to a dynamic inversion (DI) controller subject to off-nominal flight conditions.

Original languageEnglish
Title of host publicationFoundations and Applications of Intelligent Systems - The Seventh International Conference on Intelligent Systems and Knowledge Engineering, ISKE 2012, Proceedings
EditorsFuchun Sun, Hongbo Li, Tianrui Li
PublisherSpringer Verlag
Pages347-357
Number of pages11
ISBN (Electronic)9783642378287
DOIs
Publication statusPublished - 2014
Event7th International Conference on Intelligent Systems and Knowledge Engineering, ISKE 2012 with 1st International Conference on Cognitive Systems and Information Processing, CSIP 2012 - Beijing, China
Duration: 15 Dec 201217 Dec 2012

Publication series

NameAdvances in Intelligent Systems and Computing
Volume213
ISSN (Print)2194-5357

Conference

Conference7th International Conference on Intelligent Systems and Knowledge Engineering, ISKE 2012 with 1st International Conference on Cognitive Systems and Information Processing, CSIP 2012
Country/TerritoryChina
CityBeijing
Period15/12/1217/12/12

Keywords

  • Dynamic inversion
  • Flight control
  • Intelligent adaptive flight control
  • UAV

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