Integration of a Laser Precision Landing System for UAVs in All-Weather and Dynamic Environments
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Examensarbete för masterexamen
Master's Thesis
Master's Thesis
Model builders
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Abstract
Autonomous unmanned aerial vehicle (UAV) landings in GPS-denied and visually
degraded environments remain a significant challenge. Standard Global Navigation
Satellite System (GNSS) solutions are susceptible to multipath interference near
metallic structures and provide absolute rather than relative positioning, making
them unsuitable for landing on dynamic platforms. Passive visual sensors fail under
low light, fog, and direct glare, and introduce significant processing latency.
This thesis integrates an active infrared precision landing system based on the Sixdof
Space Kipa optical sensor, which operates at up to 400Hz across all lighting conditions. A decentralized control architecture was developed combining a LattePanda
Mu companion computer with a Pixhawk 6C flight controller. A custom C++ application implements a three-stage signal processing pipeline (median filter, chi-squared
outlier gate, 1D Kalman filter), weather-adaptive proportional-integral-derivative
control with gain scheduling, a hierarchical descent governor, and a finite state machine enforcing safe behavior under sensor loss and extreme conditions. Velocity
commands are transmitted to the flight controller via the MAVLink protocol.
Simulation-in-the-loop across 24 test configurations demonstrated sub-centimeter
mean landing error under calm conditions, Excellent classification (landing accuracy
within 300mm) at steady wind speeds up to 15m/s, and Excellent classification at
turbulence intensities up to 7. Under a combined worst-case scenario of 15m/s wind
and turbulence intensity 5, all five runs confirmed touchdown with a mean error of
181.4mm. The end-to-end pipeline latency was measured at 52ms, satisfying the
75ms design objective. Physical characterization of the Kipa sensor confirmed sub
3cm depth accuracy at touchdown range and near-zero position noise. Hardware
bench integration was verified through confirmed motor spin-up under algorithmic
control.
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Keywords
Unmanned Aerial Vehicles, Precision Landing, Active Infrared Tracking, PID Control, MAVLink, GPS-Denied Navigation
