Exact steering and stabilization of a PVTOL aircraft
A piecewise continuous control law for maneuvering a PVTOL aircraft is proposed. The control scheme is composed of two loops: a continuous inner state feedback one together with an outer piecewise constant one. The design procedure, based on some previous results on exact sampling and multirate tech...
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Published in | Proceedings of the 36th IEEE Conference on Decision and Control Vol. 3; pp. 2049 - 2054 vol.3 |
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Main Authors | , , , |
Format | Conference Proceeding |
Language | English |
Published |
IEEE
1997
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Subjects | |
Online Access | Get full text |
ISBN | 0780341872 9780780341876 |
ISSN | 0191-2216 |
DOI | 10.1109/CDC.1997.657068 |
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Abstract | A piecewise continuous control law for maneuvering a PVTOL aircraft is proposed. The control scheme is composed of two loops: a continuous inner state feedback one together with an outer piecewise constant one. The design procedure, based on some previous results on exact sampling and multirate techniques is briefly introduced and applied to our case study. An additional digital feedback is used to improve the robustness of the control scheme. Some simulation results are reported in order to show the effectiveness of the proposed control strategy. |
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AbstractList | A piecewise continuous control law for maneuvering a PVTOL aircraft is proposed. The control scheme is composed of two loops: a continuous inner state feedback one together with an outer piecewise constant one. The design procedure, based on some previous results on exact sampling and multirate techniques is briefly introduced and applied to our case study. An additional digital feedback is used to improve the robustness of the control scheme. Some simulation results are reported in order to show the effectiveness of the proposed control strategy. |
Author | Monaco, S. Normand-Cyrot, D. Djemai, M. Di Giamberardino, P. |
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Snippet | A piecewise continuous control law for maneuvering a PVTOL aircraft is proposed. The control scheme is composed of two loops: a continuous inner state feedback... |
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StartPage | 2049 |
SubjectTerms | Aerospace control Aircraft Control systems Digital control Linearization techniques Nonlinear control systems Nonlinear dynamical systems Nonlinear systems Sampling methods State feedback |
Title | Exact steering and stabilization of a PVTOL aircraft |
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