2022
DOI: 10.3390/app12031706
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Hardware-In-the-Loop Simulation of Time-Delayed Anti-Swing Controller for Quadrotor with Suspended Load

Abstract: Quadrotor flying vehicles with suspended loads have a lot of applications, such as mine detection and transferring loads for delivery, or through places where ground vehicles cannot reach. In these applications, the payload will be suspended underneath the vehicle and it is subjected to large oscillations due to external disturbances or the acceleration of the vehicle itself. These oscillations add additional forces and moments to the quadrotor, and this deteriorates its performance and stability. In this pape… Show more

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Cited by 4 publications
(2 citation statements)
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References 25 publications
(26 reference statements)
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“…Based on the received information, the flight control firmware decides actuator commands and controls the dynamics of the UAV and the sensor platform. PX4 firmware is already integrated to Gazebo simulation environment and have been widely used by many researchers over the years [24][25][26].…”
Section: Gazebo Simulation Environmentmentioning
confidence: 99%
“…Based on the received information, the flight control firmware decides actuator commands and controls the dynamics of the UAV and the sensor platform. PX4 firmware is already integrated to Gazebo simulation environment and have been widely used by many researchers over the years [24][25][26].…”
Section: Gazebo Simulation Environmentmentioning
confidence: 99%
“…Zhang, D. [22] presented a quadrotor anti-swing control scheme using feedforward controllers, and then used it to develop a posture visual measuring scheme based on a quadrotor suspension system model, effectively suppressing load swing. Omar, H.M. [23] applied a load-swing-angle-based anti-swing controller with delayed feedback in a hardware-in-the-loop setup to alleviate suspension load oscillations. Shi, D. [24] proposed a method for mitigating disturbances with high precision built on harmonic extended state observer (HESO), enhancing the robustness of quadrotor aircraft under suspended load influence.…”
Section: Introductionmentioning
confidence: 99%