Published at : 30 Sep 2026
Volume : IJtech
Vol 17, No 5 (2026)
DOI : https://doi.org/10.14716/ijtech.v17i5.8473
| Nada Syifa Qolbiyah | School of Electrical Engineering, Telkom University, Bandung, 40257, Indonesia |
| Muhammad Fahmi Khoirurrijal | Department of Physics, Padjadjaran University, Jatinangor, 45363, Indonesia |
| Ferry Faizal | Department of Physics, Padjadjaran University, Jatinangor, 45363, Indonesia |
| Irwan Purnama | 1. School of Electrical Engineering, Telkom University, Bandung, 40257, Indonesia 2. National Research and Innovation Agency, Bandung, 40135, Indonesia |
Precise autonomous landing of unmanned aerial vehicles in global positioning system (GPS)-denied environments remains a challenging control problem owing to image-plane measurement noise, sensor latency, and aerodynamic disturbances. This study proposes a prediction-informed landing framework that integrates a discrete-time Kalman filter tuned for ArUco marker motion in the monocular image plane with an outer-loop velocity proportional-integral-derivative controller that references the predicted state rather than the raw visual measurement. The filter operates on a state vector comprising the image-plane marker features and their temporal derivatives, supplying temporally consistent, noise-attenuated estimates throughout the landing sequence. Performance is evaluated through comparative numerical simulation and real-flight experiments under uncontrolled outdoor disturbances and benchmarked against a conventional raw-measurement pipeline. The proposed integration reduces the closed-loop steady-state positional error by 86.7% and reduces the total three-dimensional root-mean-square error relative to the baseline, with improvements of 20.8% and 21.3% in the longitudinal and lateral channels, respectively. The closed-loop settling time is preserved across all conditions, confirming that the gains primarily arise from the enhanced state estimation rather than from the control law. Real-flight results demonstrate operation under uncontrolled outdoor disturbances, with horizontal velocity tracking root-mean-square errors of 0.162 and 0.190 m/s, without requiring an additional landing sensor beyond the downward-facing monocular camera.
ArUco marker detection, Kalman state prediction, Monocular vision, Proportional-integral-derivative control, Unmanned aerial vehicle
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