Citation:
Llerena Caña, J. P., García Herrero, J., & Molina López, J. M. (2022). Error Reduction in Vision-Based Multirotor Landing System. In Sensors, 22(10), 3625-3650
xmlui.dri2xhtml.METS-1.0.item-contributor-funder:
Comunidad de Madrid Ministerio de Ciencia e Innovación (España) Universidad Carlos III de Madrid
Sponsor:
This research was partially funded by public research projects of Spanish Ministry of
Science and Innovation, references PID2020-118249RB-C22 and PDC2021-121567-C22—AEI/10.13039/
501100011033, and by the Madrid Government (Comunidad de Madrid, Spain) under the Multiannual
Agreement with UC3M in the line of Excellence of University Professors, reference EPUC3M17.
Project:
Gobierno de España. PID2020-118249RB-C22 Gobierno de España. PDC2021-121567-C22—AEI/10.13039/501100011033 Comunidad de Madrid. EPUC3M17
Keywords:
Uav
,
Autonomous landing
,
Filtering
,
Computer vision
,
Helipad context
,
Global position
,
Navigation system
,
Sitl
New applications are continuously appearing with drones as protagonists, but all of
them share an essential critical maneuver—landing. New application requirements have led the
study of novel landing strategies, in which vision systems have played and continNew applications are continuously appearing with drones as protagonists, but all of
them share an essential critical maneuver—landing. New application requirements have led the
study of novel landing strategies, in which vision systems have played and continue to play a
key role. Generally, the new applications use the control and navigation systems embedded in the
aircraft. However, the internal dynamics of these systems, initially focused on other tasks such as the
smoothing trajectories between different waypoints, can trigger undesired behaviors. In this paper,
we propose a landing system based on monocular vision and navigation information to estimate the
helipad global position. In addition, the global estimation system includes a position error correction
module by cylinder space transformation and a filtering system with a sliding window. To conclude,
the landing system is evaluated with three quality metrics, showing how the proposed correction
system together with stationary filtering improves the raw landing system.[+][-]