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Article

Load-Swing Attenuation in a Quadcopter–Payload System Through Trajectory Optimisation

School of Electrical Engineering and Telecommunications, UNSW Sydney, Sydney 2052, Australia
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Author to whom correspondence should be addressed.
Sensors 2025, 25(17), 5518; https://doi.org/10.3390/s25175518
Submission received: 3 July 2025 / Revised: 25 August 2025 / Accepted: 2 September 2025 / Published: 4 September 2025
(This article belongs to the Section Physical Sensors)

Abstract

Advancements in multi-rotor quadcopter technology and sensing capabilities have led to their increased utilisation for last-mile delivery. However, battery capacity constraints limit their use in extended-distance delivery scenarios. A visual servoing implementation is first proposed that leverages a CUDA-accelerated tag detection algorithm for real-time pose estimation of the target. A new approach is then developed to enhance quadcopter package collection by implementing a control scheme to attenuate aggressive load-swing in a payload arm that shifts from horizontal to vertical after obtaining a vertically mounted payload. The motion of the payload arm imposes a shift in the system’s centre of mass, leading to a possible instability. A non-linear control scheme is then introduced to address this problem through attenuation of the residual energy from payload oscillation. The performance of the visual servoing approach is validated through both numerical simulations and a physical quadcopter implementation, along with the performance of the load-swing attenuation through numerical simulations.
Keywords: quadcopter; load-swing attenuation; time-varying LQR; trajectory optimization; CUDA-accelerated tag detection; visual servoing quadcopter; load-swing attenuation; time-varying LQR; trajectory optimization; CUDA-accelerated tag detection; visual servoing

Share and Cite

MDPI and ACS Style

Feng, B.; Khatamianfar, A. Load-Swing Attenuation in a Quadcopter–Payload System Through Trajectory Optimisation. Sensors 2025, 25, 5518. https://doi.org/10.3390/s25175518

AMA Style

Feng B, Khatamianfar A. Load-Swing Attenuation in a Quadcopter–Payload System Through Trajectory Optimisation. Sensors. 2025; 25(17):5518. https://doi.org/10.3390/s25175518

Chicago/Turabian Style

Feng, Barry, and Arash Khatamianfar. 2025. "Load-Swing Attenuation in a Quadcopter–Payload System Through Trajectory Optimisation" Sensors 25, no. 17: 5518. https://doi.org/10.3390/s25175518

APA Style

Feng, B., & Khatamianfar, A. (2025). Load-Swing Attenuation in a Quadcopter–Payload System Through Trajectory Optimisation. Sensors, 25(17), 5518. https://doi.org/10.3390/s25175518

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