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Luis A. Sandino

dblp:123/3127 · DBLP profile ↗
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1ranked-venue papers
1as first author
0since 2021 · last 2014
—ORCID · none

Domains — the database's venue-derived domains; a paper can count in several

Artificial intelligence and machine learning · 1 · 1 first-authorSystems, architecture and hardware · 1 · 1 first-author

Expertise — from the expertise taxonomy: the topics of the expert's papers under the CCF categories. A weight counts papers with recency: 1 for a paper about the topic, 0.3 when the topic is its context, halved every five years.

Artificial intelligence
1 paper
Robot navigation and mapping · 61% Legged, aerial and field robots · 30% Motion planning and robot control · 9%

Topics — the 4 heaviest of 4, each with the papers that count most for it

TopicWeightPapersLastEvidence papers
Robotics › Legged, aerial and field robots › aerial robots
autonomous helicopter
0.212014
Tether-guided landing of unmanned helicopters without GPS sensors · ICRA 2014
Robotics › Robot navigation and mapping › localization
GPS-denied localization
0.212014
Tether-guided landing of unmanned helicopters without GPS sensors · ICRA 2014
Robotics › Robot navigation and mapping
localization
0.212014
Tether-guided landing of unmanned helicopters without GPS sensors · ICRA 2014
Robotics › Motion planning and robot control › robot control
model-based control
0.112014
Tether-guided landing of unmanned helicopters without GPS sensors · ICRA 2014

Methods — techniques the papers use, named apart from their topics

tether attitude sensing · 0.2model-based control · 0.2
YearPublicationVenuePosition
2014 Tether-guided landing of unmanned helicopters without GPS sensors
abstract
Landing of unmanned helicopters is a challenging maneuver which can be seriously affected by GPS sensor reliability. This work explores an alternative approach to GPS sensors to avoid typical drawbacks, such as inaccuracies of standalone sensors or weight/cost for Real Time Kinematic (RTK) setups. To this end, the paper studies a setup consisting of a tether linking the helicopter to the landing point. Appropriate sensing of tether attitude relative to the helicopter together with an altitude measurement, allows estimation of the helicopter's linear position relative to the landing point. Additionally, the tension exerted on the tether provides a stabilizing effect on helicopter translational dynamics. Taking into account all these considerations, a model-based control strategy is developed and implemented in the real platform. The experimental results endorse the validity of the proposed approach.
Luis A. Sandino, Daniel Santamaría, Manuel Béjar, Antidio Viguria, Konstantin Kondak, Aníbal Ollero
ICRA1