Demo Data from SIGIR 2026 / reviewers in the wild / expert
Youssef Demitri
dblp:300/4804
· DBLP profile ↗
1ranked-venue papers
1as first author
0since 2021 · last 2017
—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 · 67% Legged, aerial and field robots · 33% |
Topics — the 3 heaviest of 3, each with the papers that count most for it
| Topic | Weight | Papers | Last | Evidence papers |
|---|---|---|---|---|
Robotics › Robot navigation and mapping
state estimation |
0.3 | 1 | 2017 | Model-based wind estimation for a hovering VTOL tailsitter UAV · ICRA 2017 |
Robotics › Legged, aerial and field robots › aerial robots
unmanned aerial vehicle |
0.3 | 1 | 2017 | Model-based wind estimation for a hovering VTOL tailsitter UAV · ICRA 2017 |
Robotics › Robot navigation and mapping › state estimation
wind field estimation |
0.3 | 1 | 2017 | Model-based wind estimation for a hovering VTOL tailsitter UAV · ICRA 2017 |
Methods — techniques the papers use, named apart from their topics
kalman filter · 0.3aerodynamic modeling · 0.3
| Year | Publication | Venue | Position |
|---|---|---|---|
| 2017 | Model-based wind estimation for a hovering VTOL tailsitter UAVabstractTo many unmanned aerial vehicle (UAV) designs, the lack of information about the wind speed and direction is a limiting factor in achieving robust outdoor flight. This paper addresses the problem of wind estimation onboard a hovering vertical take-off and landing (VTOL) tailsitter UAV. The proposed estimation framework makes use of the standard onboard sensor suite: inertial measurement unit (IMU), global positioning system (GPS) and a magnetometer. No additional airspeed sensor is needed. As a result, the autopilot is provided with an estimate of the wind velocity vector in the horizontal (north-east) plane. An aerodynamic model of the vehicle has been derived and used in a Kalman filter framework to estimate the horizontal wind velocity vector in real-time. The wind estimator has been implemented onboard the UAVs autopilot and validated in real flight. As a result, we successfully obtain the direction and speed of the wind with an estimation accuracy close to the accuracy range of the ground truth measurement. Furthermore, the derived grey-box model allows to generalise the framework to different airframes. Youssef Demitri, Sebastian Verling, Thomas Stastny, Amir Melzer, Roland Siegwart |
ICRA | 1 |