Abstract

An innovative aerial manipulator with ducted fans is proposed to achieve side-on aerial manipulation tasks in a confined environment, such as canopy sampling in dense forests. The dynamic model of the novel design is studied, and on this basis a composite controller is proposed to address the challenges of arm extension and physical interaction during the manipulation process. An adaptive controller is proposed for the aerial platform to achieve good stability and tracking performance under the manipulator motion, and an impedance controller is designed for the manipulator to ensure compliance and stability during physical contact. The experimental tests validate the effectiveness of the proposed prototype structure and controller design.

Highlights

  • The application of an unmanned aerial vehicle (UAV) has become more and more extensive.The information interaction between a UAV and the environment has been unable to meet the increasing requirements

  • Figure aerial manipulator, which is mainly composed of of four parts: ducted coaxial rotor systems, of rudder systems set below the ducts, a 3four parts: twotwo ducted coaxial rotor systems, two two sets sets of rudder systems set below the ducts, a 3-DOF

  • The results show that the system with adaptive controller had good tracking performance, and the tracking accuracy could be guaranteed even when the manipulator moved in a large range

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Summary

Introduction

Figure11shows showsthe theproposed proposedtandem tandemducted ductedfan fan aerial manipulator, which is mainly composed. Figure aerial manipulator, which is mainly composed of of four parts: ducted coaxial rotor systems, of rudder systems set below the ducts, a 3four parts: twotwo ducted coaxial rotor systems, two two sets sets of rudder systems set below the ducts, a 3-DOF. DOF manipulator, and the control and power system. 5.5and kg, and manipulator, and the control and power system. The weight of theofproposed robotrobot is 5.5iskg, the the maximum grasping weight. Parameters of the aerial vehicle prototype given maximum grasping weight is 0.5iskg. TheThe keykey parameters of the aerial vehicle prototype areare given in in Table

Section 22 introduces
The difference of rotor speeds between front ducted fans causes difference
Aerial Vehicle
Dynamic Model
Kinematic Model
Environment
Control System Overview
Aerial Vehicle Controller Design
Manipulator Controller Design
Contact Test Simulation
Experimental Tests and Verification
Experiment Description
Results and and Analyses
Set the vertical wallthe at end the lateral direction of and
Conclusions
Full Text
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