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BIBTEX RIS

Robust variable structure control of a PVTOL aircraft

1997; Taylor & Francis; Volume: 28; Issue: 6 Linguagem: Inglês

10.1080/00207729708929415

ISSN

1464-5319

Autores

Xiao‐Yun Lu, Sarah K. Spurgeon, IAN POSTXETHWAITE,

Tópico(s)

Advanced Control Systems Optimization

Resumo

Abstract This paper considers the development of tracking controllers for a multi-input nonlinear non-minimum phase Planar Vertical Take-off and Landing (PVTOL)aircraft. The system is considered to be subject to bounded/sector additive external uncertainties. A dynamic sliding mode control philosophy is employed. The stability and robustness of the resulting closed-loop system is analysed. It is demonstrated that ultimate bounded tracking may be achieved with bounded inputs despite the presence of uncertainty. Additional informationNotes on contributorsXIAO-YUN LU Tel: +44 (0)16 2522 567; e-mail: xyl@sun.engg.le.ac.uk SARAH K. SPURGEON Tel: plus;44 (0)16 2522 531; e-mail: eon@leicester.ac.uk IAN POSTXETHWAITE Tel: +44 (0)16 2522 546; e-mail: ixp@leicester.ac.uk

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