Abstract
Precision landing for Unmanned Aerial Vehicles (UAVs) is an essential feature in modern UAV systems. Currently, the Return-to-Launch (RTL) method allows UAVs to land autonomously by referencing their initial GPS-based take-off coordinates. However, this approach is often inaccurate, particularly during long flight durations, as GPS data is not real-time and lacks precision. This inaccuracy in landing position can lead to potential UAV crashes, posing risks to the surroundings and incurring high costs This research proposes a new precision landing system on a moving platform to address these issues and enhance landing accuracy. The primary objective was to develop a dynamic adaptive controller that utilizes both GPS data and computer vision to achieve precise landings. Various UAV models were analyzed, with the H480 hexacopter chosen for its superior stability and responsiveness. An autonomous Husky rover, modified with a landing platform, served as the moving target. Both models were tested in the Gazebo simulator, allowing for the development, refinement, and validation of the adaptive control algorithm. The system uses GPS and vision-based inputs to guide the UAV, with pitch and roll adjustments helping it navigate smoothly toward the landing target by processing the inputs in the proposed adaptive control system. The control system’s gain coefficients were optimized to maximize landing accuracy, offset reduction, stability, responsiveness, and flight path efficiency. The fusion of GPS and vision sensors significantly improved accuracy and expanded UAV range compared to the previous literature. Simulations demonstrated that for a platform speed of 5 m/s, the proposed method achieved an average success landing rate of 90% with an average landing duration of 40 seconds and an average offset of just 0.3 meters. These results confirm the effectiveness of the adaptive controller combined with GPS and camera sensor fusion in achieving precision landings on a moving platform with significant improvement on the autonomous range, increased landing platform speed and landing accuracy. Future research should focus on fabricating this prototype to further validate the findings through experimental testing.
Metadata
| Item Type: | Thesis (PhD) |
|---|---|
| Creators: | Creators Email / ID Num. Khyasudeen, Muhammad Farris 2019659546 |
| Contributors: | Contribution Name Email / ID Num. Advisor Buniyamin, Norlida UNSPECIFIED |
| Subjects: | T Technology > TL Motor vehicles. Aeronautics. Astronautics T Technology > TL Motor vehicles. Aeronautics. Astronautics > Aeronautics. Aeronautical engineering > Aircraft |
| Divisions: | Universiti Teknologi MARA, Shah Alam > Faculty of Electrical Engineering |
| Programme: | Doctor of Philosophy (Electrical Engineering) |
| Keywords: | Unmanned aerial vehicle, UAV, Autonomous landing, Dynamic adaptive controller |
| Date: | July 2025 |
| URI: | https://ir.uitm.edu.my/id/eprint/140138 |
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