Altitude Measurement-Based Optimization of the Landing Process of UAVs

The paper addresses the loop shaping problem in the altitude control of an unmanned aerial vehicle to land the flying robot with a specific landing scenario adopted. The proposed solution is optimal, in the sense of the selected performance indices, namely minimum-time, minimum-energy, and velocity-...

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Main Authors: Dariusz Horla, Wojciech Giernacki, Jacek Cieślak, Pascual Campoy
Format: Article
Language:English
Published: MDPI AG 2021-02-01
Series:Sensors
Subjects:
UAV
Online Access:https://www.mdpi.com/1424-8220/21/4/1151
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spelling doaj-ddf190f0455d4de7a80071b1cc031e462021-02-07T00:03:48ZengMDPI AGSensors1424-82202021-02-01211151115110.3390/s21041151Altitude Measurement-Based Optimization of the Landing Process of UAVsDariusz Horla0Wojciech Giernacki1Jacek Cieślak2Pascual Campoy3Faculty of Automatic Control, Robotics and Electrical Engineering, Institute of Robotics and Machine Intelligence, Poznan University of Technology, ul. Piotrowo 3a, 60-965 Poznan, PolandFaculty of Automatic Control, Robotics and Electrical Engineering, Institute of Robotics and Machine Intelligence, Poznan University of Technology, ul. Piotrowo 3a, 60-965 Poznan, PolandFaculty of Automatic Control, Robotics and Electrical Engineering, Institute of Robotics and Machine Intelligence, Poznan University of Technology, ul. Piotrowo 3a, 60-965 Poznan, PolandComputer Vision and Aerial Robotics Group (CVAR) at Centre for Automation and Robotics (CAR), Universidad Politecnica Madrid (UPM), 28006 Madrid, SpainThe paper addresses the loop shaping problem in the altitude control of an unmanned aerial vehicle to land the flying robot with a specific landing scenario adopted. The proposed solution is optimal, in the sense of the selected performance indices, namely minimum-time, minimum-energy, and velocity-penalized related functions, achieving their minimal values, with numerous experiments conducted throughout the development and preparation to the Mohamed Bin Zayed International Robotics Challenge (MBZIRC 2020). A novel approach to generation of a reference altitude trajectory is presented, which is then tracked in a standard, though optimized, control loop. Three landing scenarios are considered, namely: minimum-time, minimum-energy, and velocity-penalized landing scenarios. The experimental results obtained with the use of the Simulink Support Package for Parrot Minidrones, and the OptiTrack motion capture system proved the effectiveness of the proposed approach.https://www.mdpi.com/1424-8220/21/4/1151optimizationenergyUAVlanding
collection DOAJ
language English
format Article
sources DOAJ
author Dariusz Horla
Wojciech Giernacki
Jacek Cieślak
Pascual Campoy
spellingShingle Dariusz Horla
Wojciech Giernacki
Jacek Cieślak
Pascual Campoy
Altitude Measurement-Based Optimization of the Landing Process of UAVs
Sensors
optimization
energy
UAV
landing
author_facet Dariusz Horla
Wojciech Giernacki
Jacek Cieślak
Pascual Campoy
author_sort Dariusz Horla
title Altitude Measurement-Based Optimization of the Landing Process of UAVs
title_short Altitude Measurement-Based Optimization of the Landing Process of UAVs
title_full Altitude Measurement-Based Optimization of the Landing Process of UAVs
title_fullStr Altitude Measurement-Based Optimization of the Landing Process of UAVs
title_full_unstemmed Altitude Measurement-Based Optimization of the Landing Process of UAVs
title_sort altitude measurement-based optimization of the landing process of uavs
publisher MDPI AG
series Sensors
issn 1424-8220
publishDate 2021-02-01
description The paper addresses the loop shaping problem in the altitude control of an unmanned aerial vehicle to land the flying robot with a specific landing scenario adopted. The proposed solution is optimal, in the sense of the selected performance indices, namely minimum-time, minimum-energy, and velocity-penalized related functions, achieving their minimal values, with numerous experiments conducted throughout the development and preparation to the Mohamed Bin Zayed International Robotics Challenge (MBZIRC 2020). A novel approach to generation of a reference altitude trajectory is presented, which is then tracked in a standard, though optimized, control loop. Three landing scenarios are considered, namely: minimum-time, minimum-energy, and velocity-penalized landing scenarios. The experimental results obtained with the use of the Simulink Support Package for Parrot Minidrones, and the OptiTrack motion capture system proved the effectiveness of the proposed approach.
topic optimization
energy
UAV
landing
url https://www.mdpi.com/1424-8220/21/4/1151
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AT wojciechgiernacki altitudemeasurementbasedoptimizationofthelandingprocessofuavs
AT jacekcieslak altitudemeasurementbasedoptimizationofthelandingprocessofuavs
AT pascualcampoy altitudemeasurementbasedoptimizationofthelandingprocessofuavs
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