A global non-linear control design for a PVTOL vehicle with aerodynamics

R. Wood; B. Cazzolato; D. Halim

doi:10.1109/CDC.2005.1583368

A global non-linear control design for a PVTOL vehicle with aerodynamics

R. Wood, B. Cazzolato, D. Halim

Research output: Chapter in Book/Conference proceeding › Conference contribution › peer-review

13 Citations (Scopus)

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.

Original language	English
Title of host publication	Proceedings of the 44th IEEE Conference on Decision and Control, and the European Control Conference, CDC-ECC '05
Pages	7478-7483
Number of pages	6
DOIs	https://doi.org/10.1109/CDC.2005.1583368
Publication status	Published - 2005
Externally published	Yes
Event	44th IEEE Conference on Decision and Control, and the European Control Conference, CDC-ECC '05 - Seville, Spain Duration: 12 Dec 2005 → 15 Dec 2005

Publication series

Name	Proceedings of the 44th IEEE Conference on Decision and Control, and the European Control Conference, CDC-ECC '05
Volume	2005

Conference

Conference	44th IEEE Conference on Decision and Control, and the European Control Conference, CDC-ECC '05
Country/Territory	Spain
City	Seville
Period	12/12/05 → 15/12/05

ASJC Scopus subject areas

General Engineering

Access to Document

10.1109/CDC.2005.1583368

Cite this

Wood, R., Cazzolato, B., & Halim, D. (2005). A global non-linear control design for a PVTOL vehicle with aerodynamics. In Proceedings of the 44th IEEE Conference on Decision and Control, and the European Control Conference, CDC-ECC '05 (pp. 7478-7483). Article 1583368 (Proceedings of the 44th IEEE Conference on Decision and Control, and the European Control Conference, CDC-ECC '05; Vol. 2005). https://doi.org/10.1109/CDC.2005.1583368

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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.",

author = "R. Wood and B. Cazzolato and D. Halim",

note = "Copyright: Copyright 2008 Elsevier B.V., All rights reserved.; 44th IEEE Conference on Decision and Control, and the European Control Conference, CDC-ECC '05 ; Conference date: 12-12-2005 Through 15-12-2005",

year = "2005",

doi = "10.1109/CDC.2005.1583368",

language = "English",

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series = "Proceedings of the 44th IEEE Conference on Decision and Control, and the European Control Conference, CDC-ECC '05",

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Wood, R, Cazzolato, B & Halim, D 2005, A global non-linear control design for a PVTOL vehicle with aerodynamics. in Proceedings of the 44th IEEE Conference on Decision and Control, and the European Control Conference, CDC-ECC '05., 1583368, Proceedings of the 44th IEEE Conference on Decision and Control, and the European Control Conference, CDC-ECC '05, vol. 2005, pp. 7478-7483, 44th IEEE Conference on Decision and Control, and the European Control Conference, CDC-ECC '05, Seville, Spain, 12/12/05. https://doi.org/10.1109/CDC.2005.1583368

A global non-linear control design for a PVTOL vehicle with aerodynamics. / Wood, R.; Cazzolato, B.; Halim, D.
Proceedings of the 44th IEEE Conference on Decision and Control, and the European Control Conference, CDC-ECC '05. 2005. p. 7478-7483 1583368 (Proceedings of the 44th IEEE Conference on Decision and Control, and the European Control Conference, CDC-ECC '05; Vol. 2005).

Research output: Chapter in Book/Conference proceeding › Conference contribution › peer-review

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AB - 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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Wood R, Cazzolato B, Halim D. A global non-linear control design for a PVTOL vehicle with aerodynamics. In Proceedings of the 44th IEEE Conference on Decision and Control, and the European Control Conference, CDC-ECC '05. 2005. p. 7478-7483. 1583368. (Proceedings of the 44th IEEE Conference on Decision and Control, and the European Control Conference, CDC-ECC '05). doi: 10.1109/CDC.2005.1583368

A global non-linear control design for a PVTOL vehicle with aerodynamics

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