Fixed-Wing Unmanned Aerial Vehicle 3D-Model-Based Tracking for Autonomous Landing

Author:

Pessanha Santos Nuno12ORCID,Lobo Victor34ORCID,Bernardino Alexandre2ORCID

Affiliation:

1. Portuguese Military Research Center (CINAMIL), Portuguese Military Academy (Academia Militar), R. Gomes Freire 203, 1169-203 Lisbon, Portugal

2. Institute for Systems and Robotics (ISR), Instituto Superior Técnico (IST), 1049-001 Lisbon, Portugal

3. Portuguese Navy Research Center (CINAV), Portuguese Naval Academy (Escola Naval), Alfeite, 2800-001 Almada, Portugal

4. NOVA Information Management School (NOVA IMS), Universidade Nova de Lisboa, 1070-312 Lisbon, Portugal

Abstract

The vast increase in the available computational capability has allowed the application of Particle-Filter (PF)-based approaches for monocular 3D-model-based tracking. These filters depend on the computation of a likelihood function that is usually unavailable and can be approximated using a similarity metric. We can use temporal filtering techniques between filter iterations to achieve better results when dealing with this suboptimal approximation, which is particularly important when dealing with the Unmanned Aerial Vehicle (UAV) model symmetry. The similarity metric evaluation time is another critical concern since we usually want a real-time implementation. We explored, tested, and compared with the same dataset two different types of PFs, (i) an Unscented Bingham Filter (UBiF) and (ii) an Unscented Bingham–Gauss Filter (UBiGaF), using pose optimization in both implementations. Using optimization steps between iterations increases the convergence capability of the filter and decreases the obtained error. A new tree-based similarity metric approach is also explored based on the Distance Transform (DT), allowing a faster evaluation of the possibilities without losing accuracy. The results showed that the obtained pose estimation error is compatible with the automatic landing requirements.

Publisher

MDPI AG

Subject

Artificial Intelligence,Computer Science Applications,Aerospace Engineering,Information Systems,Control and Systems Engineering

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