Nonlinear automatic landing control of unmanned aerial vehicles on moving platforms via a 3D laser radar

This paper presents a motion tracking and control system for automatically landing Unmanned Aerial Vehicles (UAVs) on an oscillating platform using Laser Radar (LADAR) observations. The system itself is assumed to be mounted on a ship deck. A full nonlinear mathematical model is first introduced for...

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Main Authors: Hervas, Jaime Rubio, Reyhanoglu, Mahmut, Tang, Hui
Other Authors: School of Mechanical and Aerospace Engineering
Format: Conference or Workshop Item
Language:English
Published: 2016
Subjects:
UAV
Online Access:https://hdl.handle.net/10356/81916
http://hdl.handle.net/10220/39711
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-819162023-03-04T17:08:04Z Nonlinear automatic landing control of unmanned aerial vehicles on moving platforms via a 3D laser radar Hervas, Jaime Rubio Reyhanoglu, Mahmut Tang, Hui School of Mechanical and Aerospace Engineering AIP Conference Proceedings UAV Sliding mode Nonlinear control State estimation Extended Kalman filter Laser radar Landing This paper presents a motion tracking and control system for automatically landing Unmanned Aerial Vehicles (UAVs) on an oscillating platform using Laser Radar (LADAR) observations. The system itself is assumed to be mounted on a ship deck. A full nonlinear mathematical model is first introduced for the UAV. The ship motion is characterized by a Fourier transform based method which includes a realistic characterization of the sea waves. LADAR observation models are introduced and an algorithm to process those observations for yielding the relative state between the vessel and the UAV is presented, from which the UAV's state relative to an inertial frame can be obtained and used for feedback purposes. A sliding mode control algorithm is derived for tracking a landing trajectory defined by a set of desired waypoints. An extended Kalman filter (EKF) is proposed to account for process and observation noises in the design of a state estimator. The effectiveness of the control algorithm is illustrated through a simulation example. Published version 2016-01-19T07:20:33Z 2019-12-06T14:42:59Z 2016-01-19T07:20:33Z 2019-12-06T14:42:59Z 2014 Conference Paper Hervas, J. R., Reyhanoglu, M., & Tang, H. (2014). Nonlinear automatic landing control of unmanned aerial vehicles on moving platforms via a 3D laser radar. AIP Conference Proceedings, 907-917. https://hdl.handle.net/10356/81916 http://hdl.handle.net/10220/39711 10.1063/1.4904663 en © 2014 American Institute of Physics. This paper was published in AIP Conference Proceedings and is made available as an electronic reprint (preprint) with permission of American Institute of Physics. The published version is available at: [http://dx.doi.org/10.1063/1.4904663]. One print or electronic copy may be made for personal use only. Systematic or multiple reproduction, distribution to multiple locations via electronic or other means, duplication of any material in this paper for a fee or for commercial purposes, or modification of the content of the paper is prohibited and is subject to penalties under law. 11 p. application/pdf
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic UAV
Sliding mode
Nonlinear control
State estimation
Extended Kalman filter
Laser radar
Landing
spellingShingle UAV
Sliding mode
Nonlinear control
State estimation
Extended Kalman filter
Laser radar
Landing
Hervas, Jaime Rubio
Reyhanoglu, Mahmut
Tang, Hui
Nonlinear automatic landing control of unmanned aerial vehicles on moving platforms via a 3D laser radar
description This paper presents a motion tracking and control system for automatically landing Unmanned Aerial Vehicles (UAVs) on an oscillating platform using Laser Radar (LADAR) observations. The system itself is assumed to be mounted on a ship deck. A full nonlinear mathematical model is first introduced for the UAV. The ship motion is characterized by a Fourier transform based method which includes a realistic characterization of the sea waves. LADAR observation models are introduced and an algorithm to process those observations for yielding the relative state between the vessel and the UAV is presented, from which the UAV's state relative to an inertial frame can be obtained and used for feedback purposes. A sliding mode control algorithm is derived for tracking a landing trajectory defined by a set of desired waypoints. An extended Kalman filter (EKF) is proposed to account for process and observation noises in the design of a state estimator. The effectiveness of the control algorithm is illustrated through a simulation example.
author2 School of Mechanical and Aerospace Engineering
author_facet School of Mechanical and Aerospace Engineering
Hervas, Jaime Rubio
Reyhanoglu, Mahmut
Tang, Hui
format Conference or Workshop Item
author Hervas, Jaime Rubio
Reyhanoglu, Mahmut
Tang, Hui
author_sort Hervas, Jaime Rubio
title Nonlinear automatic landing control of unmanned aerial vehicles on moving platforms via a 3D laser radar
title_short Nonlinear automatic landing control of unmanned aerial vehicles on moving platforms via a 3D laser radar
title_full Nonlinear automatic landing control of unmanned aerial vehicles on moving platforms via a 3D laser radar
title_fullStr Nonlinear automatic landing control of unmanned aerial vehicles on moving platforms via a 3D laser radar
title_full_unstemmed Nonlinear automatic landing control of unmanned aerial vehicles on moving platforms via a 3D laser radar
title_sort nonlinear automatic landing control of unmanned aerial vehicles on moving platforms via a 3d laser radar
publishDate 2016
url https://hdl.handle.net/10356/81916
http://hdl.handle.net/10220/39711
_version_ 1759857424325410816