Study on roll angle control for hovering tilt rotor aircraft on one side thrust reduction

Yasuhiro Osa, Shigeru Uchikado, Kanya Tanaka

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

In this study a synthesis of flight control system which is able to control the roll angle of hovering Tilt Rotor Aircraft (TRA) on one side thrust reduction, which seriously affects the stability of TRA motion, is proposed. Basically this flight control system is constructed with roll angle feedback as stability augmentation method and P or PI control as controllability augmentation method.

Original languageEnglish
Title of host publicationCACS 2014 - 2014 International Automatic Control Conference, Conference Digest
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages128-131
Number of pages4
ISBN (Electronic)9781479945849
DOIs
Publication statusPublished - 28 Apr 2014
Event2014 International Automatic Control Conference, CACS 2014 - Kaohsiung, Taiwan, Province of China
Duration: 26 Nov 201428 Nov 2014

Publication series

NameCACS 2014 - 2014 International Automatic Control Conference, Conference Digest

Conference

Conference2014 International Automatic Control Conference, CACS 2014
CountryTaiwan, Province of China
CityKaohsiung
Period26/11/1428/11/14

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  • Cite this

    Osa, Y., Uchikado, S., & Tanaka, K. (2014). Study on roll angle control for hovering tilt rotor aircraft on one side thrust reduction. In CACS 2014 - 2014 International Automatic Control Conference, Conference Digest (pp. 128-131). [7097175] (CACS 2014 - 2014 International Automatic Control Conference, Conference Digest). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CACS.2014.7097175