A global non-linear control design for a PVTOL vehicle with aerodynamics
Date
2005
Authors
Wood, R.
Cazzolato, B.
Halim, D.
Editors
Camacho, E.
Advisors
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Conference paper
Citation
Proceedings of the 44th IEEE Conference on Decision and Control and the European Control Conference CDC-ECC 2005 / E. F. Camacho (ed.): pp.7478-7483
Statement of Responsibility
R. Wood, B. Cazzolato, D. Halim
Conference Name
IEEE Conference on Decision and Control (44th : 2005 : Seville, Spain)
Abstract
Non-linear stabilisation and control of a PVTOL vehicle has received much attention in the literature for the low speed case, where aerodynamic effects can be neglected. In this paper, a non-linear control design is presented for a three degree of freedom "Hovering Rocket" with aerodynamic effects included, such that the controller remains functional at high speeds. Control design is based on a non-linear, decoupling change of coordinates presented by many authors in the past. The decoupled system is then controlled using an optimised cascade approach.
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© Copyright 2006 IEEE