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Disturbance and uncertainty control method based on operation type flying robot

A flying robot and control method technology, applied in aircraft, non-electric variable control, motor vehicles, etc., can solve problems such as the interaction force and torque interference between the rotorcraft and the manipulator

Active Publication Date: 2020-11-24
FUZHOU UNIV
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  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The interaction forces and torques between the rotorcraft and the robotic arm then become disturbances

Method used

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  • Disturbance and uncertainty control method based on operation type flying robot
  • Disturbance and uncertainty control method based on operation type flying robot
  • Disturbance and uncertainty control method based on operation type flying robot

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Embodiment Construction

[0121] The invention will be further described below with reference to the accompanying drawings and examples.

[0122] Please refer to figure 2 The present invention provides a method of perturbation and uncertainty control based on job type flight robots, including the following steps:

[0123] Step S1: Constructing a work type flying robot system composed of a four-rotor aircraft and a three-degree-freedom active robot, and modeling its kinematics and kinetic models;

[0124] Step S2: Using geometric control method, in the case of mechanical arm dynamics, the position and posture of the rotorvers are tracked by the rotor aircraft;

[0125] Step S3: Using the modelless active robotic arm control, overcoming uncertainty and external interference brought by the rotorcraft and system working environment;

[0126] Step S4: Lyapunov function controlled by the work type flight robot;

[0127] Step S5: Based on the Lyapunov function, the stability analysis of the rotorcraft of the job ...

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Abstract

The invention relates to a disturbance and uncertainty control method based on an operation type flying robot, and the method comprises the following steps: S1, constructing an operation type flying robot system composed of a four-rotor aircraft and a three-degree-of-freedom active mechanical arm, and carrying out the modeling analysis of a kinematics and dynamics model of the operation type flying robot system; S2, tracking the position and attitude of the four-rotor aircraft by adopting a geometric control method under the condition that the dynamics of the mechanical arm influences the four-rotor aircraft; S3, adopting model-free active mechanical arm control to overcome uncertainty and external interference caused by the working environment of the four-rotor aircraft and the system; S4, constructing a Lyapunov function used for controlling the operation type flying robot; and S5, based on the Lyapunov function, analyzing the stability of the rotor aircraft of the operation type flying robot system, and further controlling the operation type flying robot system to fly stably. According to the method, the control precision of the operation type flying robot under disturbance anduncertainty can be effectively improved.

Description

Technical field [0001] The present invention relates to the dynamic control of operation type flight robots involving a perturbation and uncertainty control method based on job type flight robot. Background technique [0002] In recent years, with the development of automation technology and the development of drones, researchers attempt to add an active robot to the rotorbeaux to build a combined system. This novel robot structure greatly enriches the potential application of the rotorfire, which can perform various tasks in harsh environments, such as crawling and handling equipment in boys, air detection and disposal of dangerous goods. A variety of job type flying robot mechanical structures have been developed to deal with difficult tasks in complex environments. In order to establish a docking system, the prototype docking system of the acrylonitrile butrene styrene (ABS) material 3D is mounted on the drone. The manified, a soft and light arms system is mounted on the rotor...

Claims

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Application Information

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IPC IPC(8): G05D1/08G05D1/10B64C39/02
CPCG05D1/0825G05D1/102B64C39/02Y02T90/00
Inventor 陈彦杰梁嘉诚赖宁斌何炳蔚林立雄
Owner FUZHOU UNIV
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