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Trajectory Generation and Control of a Quadrotor with Slung Payload Considering Swing Suppression and Cable Collision Avoidance

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dc.contributor.advisor김유단-
dc.contributor.author이준수-
dc.date.accessioned2018-05-29T03:17:36Z-
dc.date.available2018-05-29T03:17:36Z-
dc.date.issued2018-02-
dc.identifier.other000000150524-
dc.identifier.urihttps://hdl.handle.net/10371/141409-
dc.description학위논문 (석사)-- 서울대학교 대학원 : 공과대학 기계항공공학부, 2018. 2. 김유단.-
dc.description.abstractIn this thesis, a trajectory generation algorithm is proposed for a quadrotor with slung payload. There exist two major issues of the slung payload: cable collision and payload swing. Previous studies tried to circumvent cable collision effect by performing conservative payload lifting, that is by placing the quadrotor at the top of the payload and lifting it gently. In this paper, the state jump occurs at cable collision is limited to its magnitude by aligning the velocity vector of the quadrotor with the position vector between the vehicle and the load. Therefore, the trajectory can be generated without dividing it into several discrete modes. Swing of the payload should be suppressed to avoid undesirable potential instabilities throughout the mission. Therefore, trajectory suppressing the swing is generated by minimizing the derivative of the tension over the whole mission. The reference trajectory suppressing the payload swing is generated. Rapidly-exploring Random Tree algorithm is used for generating intermediate waypoints between initial position and final position. By planning the path in advance, limitations on sensor and controller of the system can be relieved. The proposed method can make quadrotor follow the reference trajectory without knowing the current state information of the payload, thereby the payload can also follow the swing suppressing trajectory. Numerical simulation is performed to demonstrate the performance of the proposed algorithm.-
dc.description.tableofcontentsChapter1 1
1 Introduction 1
1.1 Background and Motivation 1
1.2 Literature Survey 3
1.3 Objectives 4
1.4 Research Contribution 5
1.5 Thesis Organization 5
2 Problem Statement 6
2.1 Slung-payload quadrotor system 6
2.2 System Dynamics 7
2.3 Cable Collision 9
2.3.1 Lifting Maneuver 11
2.3.2 Landing Maneuver 14
2.4 Payload Swing 16
2.5 Cable Dynamics 17
2.6 Motor Dynamics 18
3 Trajectory Generation and Trajectory Tracking Controller 20
3.1 Waypoint Generation with RRT 20
3.2 Lifting and Landing Constraints 23
3.3 Trajectory Generation for the Payload 23
3.3.1 Swing Suppression Trajectory 23
3.3.2 Time of Arrivals at Waypoints 27
3.3.3 Determining Coecients: Constrained QP 28
3.3.4 Determining Coecients: Unconstrained QP 31
3.4 Quadrotor Trajectory 32
3.5 Trajectory Tracking Controller 34
4 Numerical Simulation 37
4.1 Simulation 1: Reference comparison 39
4.2 Simulation II: Fast Mission 55
4.3 Simulation III: Touch-and-Go Mission 62
5 Conclusions 70
References 72
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dc.formatapplication/pdf-
dc.format.extent46855122 bytes-
dc.format.mediumapplication/pdf-
dc.language.isoen-
dc.publisher서울대학교 대학원-
dc.subjectQuadrotor-
dc.subjectSlung Payload-
dc.subjectPath Planning-
dc.subjectCable Collision-
dc.subjectPayload Swing-
dc.subject.ddc621-
dc.titleTrajectory Generation and Control of a Quadrotor with Slung Payload Considering Swing Suppression and Cable Collision Avoidance-
dc.typeThesis-
dc.description.degreeMaster-
dc.contributor.affiliation공과대학 기계항공공학부-
dc.date.awarded2018-02-
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