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A Design Method of Control System of Flying Robot Carrying Redundant Manipulator

A technology of flying robot and design method, which is applied in the direction of aircraft, manipulator, program control manipulator, etc., and can solve the problem that the UAV controller is difficult to meet expectations.

Active Publication Date: 2020-11-24
SOUTH CHINA UNIV OF TECH
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  • Abstract
  • Description
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  • Application Information

AI Technical Summary

Problems solved by technology

Due to the influence of the complexity of the actual application environment and the diversity of task conditions, the traditional UAV controller designed based on the PID closed-loop control algorithm and the corresponding improved control algorithm is gradually difficult to meet people's expectations.

Method used

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  • A Design Method of Control System of Flying Robot Carrying Redundant Manipulator
  • A Design Method of Control System of Flying Robot Carrying Redundant Manipulator
  • A Design Method of Control System of Flying Robot Carrying Redundant Manipulator

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Embodiment

[0077] Such as figure 1 As shown, a design method of a flying robot control system with redundant manipulators is specifically aimed at the design of two aspects of the aircraft adaptive stable flight controller and the redundant manipulator controller, including the following steps:

[0078] S1. According to the real-time flight operation data of the flying robot itself obtained by the attitude sensor mounted on the flying robot and the corresponding height and position sensors, the dynamic modeling of the flying robot with redundant mechanical arms is carried out;

[0079] S2. According to the dynamic equation of the flying robot established in step S1, design a horizontal position controller, a height controller, and an attitude controller, and introduce a virtual control quantity from the lowest order differential equation of the system, and adopt a method based on the Lyapunov stability principle Pushback method, design the virtual control that meets the system stability ...

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Abstract

The invention discloses a design method of a control system of a flying robot carrying a redundancy mechanical arm. The design method is used for achieving the design of a six-rotor aircraft self-adaptive stabilized flight controller and a redundancy mechanical arm controller, and mainly comprises the following steps that dynamics modeling is conducted on the flying robot carrying the redundancy mechanical arm according to the flight real-time operation data; then a position controller, a height controller and a posture controller are designed according to a modeling equation, and trajectory tracking treatment is conducted by use of a pushback method based on the liapunov stability theory; self-adaptive treatment is conducted, and therefore the design of the aircraft self-adaptive stabilized flight controller can be accomplished; and the mechanical arm motion planning scheme design and the quadratic programming design are adopted by the redundancy mechanical arm motion planning controller. The self-adaptive pushback design method can rapidly and accurately track the target trajectory of an aircraft in real time, and improves the robustness and the stability of the system.

Description

technical field [0001] The invention belongs to the field of flying robot control system design, in particular to a design method of a flying robot control system with redundant mechanical arms based on adaptive pushback design. Background technique [0002] In recent years, countries all over the world are vigorously developing multi-rotor aircraft, which have been widely used in both military and civilian applications. Compared with traditional aircraft, multi-rotor aircraft has the advantages of smaller size, lower cost, strong maneuverability, fixed-point hovering, vertical take-off and landing, and flying in various attitudes. It can be used in military affairs with high efficiency. It is used for reconnaissance and surveillance, etc., and for civilian use, such as power line inspection. With the rapid development of drone technology, radar, laser, sonar and other instruments and equipment can be equipped on drones to complete specific tasks. With the advancement of ro...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B25J9/16B64C27/02B64C27/54
CPCB25J9/16B25J9/1664B64C27/02B64C27/54
Inventor 张智军吴春台翁卓荣林亮洪谢楷俊郑陆楠
Owner SOUTH CHINA UNIV OF TECH
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