2018 IEEE/RSJ International Conference on Intelligent Robots and Systems (IROS) 2018
DOI: 10.1109/iros.2018.8593952
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Decentralized Motion Control in a Cabled-based Multi-drone Load Transport System

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Cited by 13 publications
(8 citation statements)
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“…depicts the evolution of the quadrotor attitude when the two control laws are applied. In the left column, the results for the proposed control law are shown, whereas the right column portrays the results using (17). In both cases, the first subplot of each column shows the time evolution for the scalar component of the desired and current quaternion.…”
Section: Quaternion and Angular Velocity Evolutionmentioning
confidence: 99%
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“…depicts the evolution of the quadrotor attitude when the two control laws are applied. In the left column, the results for the proposed control law are shown, whereas the right column portrays the results using (17). In both cases, the first subplot of each column shows the time evolution for the scalar component of the desired and current quaternion.…”
Section: Quaternion and Angular Velocity Evolutionmentioning
confidence: 99%
“…Once the disturbance vanishes, the control loop is closed, and the aircraft performs as desired. Finally, the control (torque) signal is shown in Figure 6 for both approaches ( 16) and (17). Note that the constraints on the control magnitude are respected.…”
Section: Disturbance Estimation and Rejectionmentioning
confidence: 99%
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“…However, the above rigid joint methods will limit the size of UAVs and payload. In addition, some cooperative methods for transferring a payload fixed with cable by multiple UAVs [11,12,14,15] was proposed, which has a high degree of freedom in selecting the number and size of UAVs and payload. These research methods mainly use PD control for basic control.…”
Section: Introductionmentioning
confidence: 99%
“…Approaches to inertia compensation and vibration suppression are roughly classified into two types. The first is a method of accurately modelling and controlling a control object, which requires information such as attitude and acceleration, cable angle, and payload mass [11,12,14]. The second method is to use an observer to compensate for disturbance.…”
Section: Introductionmentioning
confidence: 99%