Optimal switching control for Morphing aircraft with Aerodynamic Uncertainty

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

7 Citations (Scopus)

Abstract

A novel optimal switching attitude controller for variable-span and variable-sweep morphing aircraft is proposed based on approximate dynamic programming (ADP) and non-linear disturbance observer (NDO). Value iteration (VI) based ADP is utilized to solve the infinite horizon switching control problem with deterministic dynamics. To cope with the aero-dynamic uncertainty in morphing aircraft, a NDO and extra control for switching system are designed to compensate the disturbance caused by model uncertainty. Nonlinear simulations are performed to demonstrate the effectiveness of the proposed scheme. Simulation results show that the proposed controller can coordinate morphing control and flight control to achieve optimal maneuvering under aerodynamic uncertainty.

Original languageEnglish
Title of host publication2020 IEEE 16th International Conference on Control and Automation, ICCA 2020
PublisherIEEE Computer Society
Pages1167-1172
Number of pages6
ISBN (Electronic)9781728190938
DOIs
Publication statusPublished - 9 Oct 2020
Event16th IEEE International Conference on Control and Automation, ICCA 2020 - Virtual, Sapporo, Hokkaido, Japan
Duration: 9 Oct 202011 Oct 2020

Publication series

NameIEEE International Conference on Control and Automation, ICCA
Volume2020-October
ISSN (Print)1948-3449
ISSN (Electronic)1948-3457

Conference

Conference16th IEEE International Conference on Control and Automation, ICCA 2020
Country/TerritoryJapan
CityVirtual, Sapporo, Hokkaido
Period9/10/2011/10/20

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