Fixed-time autonomous shipboard landing control of a helicopter with external disturbances

This paper presents a new fixed-time control algorithm to enable autonomous landing of a helicopter onto the ship's deck in the presence of parametric uncertainties and external disturbances. A nonsingular terminal sliding control is implemented as an integral part of the fixed-time control sch...

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Main Authors: Huang, Yanting, Zhu, Ming, Zheng, Zewei, Feroskhan, Mir
Other Authors: School of Mechanical and Aerospace Engineering
Format: Article
Language:English
Published: 2020
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Online Access:https://hdl.handle.net/10356/144524
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-1445242023-03-04T17:17:46Z Fixed-time autonomous shipboard landing control of a helicopter with external disturbances Huang, Yanting Zhu, Ming Zheng, Zewei Feroskhan, Mir School of Mechanical and Aerospace Engineering Engineering::Mechanical engineering Helicopter Shipboard Landing This paper presents a new fixed-time control algorithm to enable autonomous landing of a helicopter onto the ship's deck in the presence of parametric uncertainties and external disturbances. A nonsingular terminal sliding control is implemented as an integral part of the fixed-time control scheme, that guarantees the convergence of system errors to zero in a fixed settling time, however, without the consideration of disturbances. Subsequently, a fixed-time disturbance observer is incorporated into the control structure to efficiently estimate the lumped disturbances including modeling inaccuracies and external perturbations, while reducing the undesired chattering in the control inputs effectively as well. By establishing a relative motion model between the helicopter and the ship, the shipboard landing problem is converted from a general trajectory tracking problem to a more favorable stabilization problem. Based on the fixed-time control scheme in the relative motion model, a relative position controller (RPC) and a relative attitude-altitude controller (RAC) are formulated to guide the helicopter in a dual-phase landing sequence. The RPC will first be implemented to direct the helicopter from its initial position to a hover position above the ship. The next phase involves the application of RAC to guide the helicopter to descend steadily on the ship. Numerical comparative simulations are also carried out to validate the remarkable performance of the proposed control approach. Accepted version 2020-11-11T03:57:15Z 2020-11-11T03:57:15Z 2018 Journal Article Huang, Y., Zhu, M., Zheng, Z., & Feroskhan, M. (2019). Fixed-time autonomous shipboard landing control of a helicopter with external disturbances. Aerospace Science and Technology, 84, 18–30. doi:10.1016/j.ast.2018.07.032 1270-9638 https://hdl.handle.net/10356/144524 10.1016/j.ast.2018.07.032 84 18 30 en Aerospace Science and Technology © 2018 Elsevier Masson SAS. All rights reserved. This paper was published in Aerospace Science and Technology and is made available with permission of Elsevier Masson SAS. application/pdf
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic Engineering::Mechanical engineering
Helicopter
Shipboard Landing
spellingShingle Engineering::Mechanical engineering
Helicopter
Shipboard Landing
Huang, Yanting
Zhu, Ming
Zheng, Zewei
Feroskhan, Mir
Fixed-time autonomous shipboard landing control of a helicopter with external disturbances
description This paper presents a new fixed-time control algorithm to enable autonomous landing of a helicopter onto the ship's deck in the presence of parametric uncertainties and external disturbances. A nonsingular terminal sliding control is implemented as an integral part of the fixed-time control scheme, that guarantees the convergence of system errors to zero in a fixed settling time, however, without the consideration of disturbances. Subsequently, a fixed-time disturbance observer is incorporated into the control structure to efficiently estimate the lumped disturbances including modeling inaccuracies and external perturbations, while reducing the undesired chattering in the control inputs effectively as well. By establishing a relative motion model between the helicopter and the ship, the shipboard landing problem is converted from a general trajectory tracking problem to a more favorable stabilization problem. Based on the fixed-time control scheme in the relative motion model, a relative position controller (RPC) and a relative attitude-altitude controller (RAC) are formulated to guide the helicopter in a dual-phase landing sequence. The RPC will first be implemented to direct the helicopter from its initial position to a hover position above the ship. The next phase involves the application of RAC to guide the helicopter to descend steadily on the ship. Numerical comparative simulations are also carried out to validate the remarkable performance of the proposed control approach.
author2 School of Mechanical and Aerospace Engineering
author_facet School of Mechanical and Aerospace Engineering
Huang, Yanting
Zhu, Ming
Zheng, Zewei
Feroskhan, Mir
format Article
author Huang, Yanting
Zhu, Ming
Zheng, Zewei
Feroskhan, Mir
author_sort Huang, Yanting
title Fixed-time autonomous shipboard landing control of a helicopter with external disturbances
title_short Fixed-time autonomous shipboard landing control of a helicopter with external disturbances
title_full Fixed-time autonomous shipboard landing control of a helicopter with external disturbances
title_fullStr Fixed-time autonomous shipboard landing control of a helicopter with external disturbances
title_full_unstemmed Fixed-time autonomous shipboard landing control of a helicopter with external disturbances
title_sort fixed-time autonomous shipboard landing control of a helicopter with external disturbances
publishDate 2020
url https://hdl.handle.net/10356/144524
_version_ 1759854616226299904