Application of ICC LPV control to a blended-wing-body airplane with guaranteed$ {\mathcal{H}}_{\infty }$performance

Al-Jiboory, Ali K.; Su, Weihua; Swei, Sean S.-M.; Zhu, Guoming G.; He, Tianyi

doi:10.1016/j.ast.2018.07.046

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Application of ICC LPV control to a blended-wing-body airplane with guaranteed${\mathcal{H}}_{\infty }$performance

Author(s): Tianyi He , Ali K. Al-Jiboory , Guoming G. Zhu , Sean S.-M. Swei , Weihua Su

Publication date Created: October 2018

Publication date (Print): October 2018

Journal: Aerospace Science and Technology

Publisher: Elsevier BV

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Title: Aerospace Science and Technology

Abbreviated Title: Aerospace Science and Technology

Publisher: Elsevier BV

ISSN (Print): 12709638

Publication date Created: October 2018

Publication date (Print): October 2018

Volume: 81

Pages: 88-98

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DOI: 10.1016/j.ast.2018.07.046

SO-VID: d16dc9e5-ad88-4d97-9f9c-e080267c77f2

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https://www.elsevier.com/tdm/userlicense/1.0/

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Application of ICC LPV control to a blended-wing-body airplane with guaranteed\({\mathcal{H}}_{\infty }\)performance

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