An obstacle avoidance method for unmanned aerial vehicle based on double-rotation lyapunov vector field

A technology of unmanned aerial vehicles and vector fields, applied in three-dimensional position/course control, etc., can solve problems that are not suitable for dynamic obstacle avoidance planning, difficult, and do not meet dynamic constraints

Active Publication Date: 2020-06-02
NAVAL AVIATION UNIV
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Among them, the heuristic algorithm can quickly plan a feasible trajectory from the starting point to the target point, but this type of method does not consider the maneuverability of the unmanned aerial vehicle, the planned trajectory is not flyable and needs to be carried out on the planned trajectory. The shortcomings of smoothing processing; and the method based on graph theory can seek the obstacle avoidance path from the starting point to the target point by traversing the space, but this type of method not only does not satisfy the dynamic constraints, but also needs to be adjusted once the task space changes. Space retraversal is not suitable for the obstacle avoidance planning of dynamic obstacles; while the geometric method can meet the flight dynamics constraints such as turning radius, but it can only avoid obstacles for static targets, and find a suitable obstacle avoidance tool for avoiding dynamic obstacles. point is very difficult
[0004] In summary, although the above three types of methods have their own advantages, they cannot meet the requirements of dynamic constraints and dynamic obstacle avoidance at the same time.

Method used

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  • An obstacle avoidance method for unmanned aerial vehicle based on double-rotation lyapunov vector field
  • An obstacle avoidance method for unmanned aerial vehicle based on double-rotation lyapunov vector field
  • An obstacle avoidance method for unmanned aerial vehicle based on double-rotation lyapunov vector field

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Experimental program
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Effect test

Embodiment 1

[0109] Based on the single obstacle avoidance model, the obstacle avoidance simulation verification of a single obstacle is carried out. The simulation parameters are shown in Table 1:

[0110] Table 1 Simulation parameters

[0111]

[0112] The obstacle avoidance of a single static obstacle is first verified. Figure 13 In , the obstacle coordinates are on the connecting line between the UAV and the target. At this time, the obstacle avoidance effects on both sides are the same. When the obstacle coordinates are (13, 9), according to the method in step S3, it is determined that the left side of the UAV is the optimal obstacle avoidance direction, and the rotation direction of the vector field is clockwise. When the obstacle coordinates are (9, 13), the conclusion is opposite to that of (13, 9). In order to verify the success of obstacle avoidance and the dynamic constraints of the UAV, the obstacle avoidance in the counterclockwise direction of the obstacle coordinates (...

Embodiment 2

[0114] Next, the obstacle avoidance of a single dynamic obstacle is verified. Obstacle avoidance of dynamic targets is a key point of the obstacle avoidance problem. The initial position of the obstacle is (2.3,19.7), and its movement direction angle is -45 ° , after the unmanned aerial vehicle detects an obstacle, it performs obstacle avoidance, and then uses the method of step S4 to determine whether the obstacle avoidance is successful. The simulation result shows that at t=97, it is determined that the obstacle avoidance is successful. A single dynamic obstacle avoidance track such as Figure 14 shown.

[0115] In order to illustrate the accuracy of the dynamic obstacle avoidance method more intuitively, the simulation results of two obstacle avoidance directions are compared for dynamic obstacles. The radius of the obstacle safety circle in the simulation is R safe = 3.3km, the simulation results are shown in Table 2:

[0116] Table 2 Comparison of simulation results ...

Embodiment 3

[0121] In order to verify the performance of the method of the present invention, the method based on Dubins path and the artificial potential field method are used as comparative verification. Consider the static obstacle avoidance of the starting point coordinates (0,0), the target point coordinates (20,20), the obstacle parameters (11,11,3) and the starting point (2.3,19.7), and the speed size is 0.141 , the velocity direction is -45 ° dynamic obstacles for obstacle avoidance. Since the position of the static obstacle is on the line between the starting point and the target point, there is a minimum point, so the improved artificial potential field method is used to avoid the obstacle by adding a disturbance factor to overcome the local minimum point; according to the UAV maneuvering in Table 1 Performance constraints, it can be known that the minimum turning radius R of the UAV in the Dubins path min =4. The simulation results are as follows:

[0122] Table 3 Simulatio...

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Abstract

The invention discloses an unmanned aerial vehicle obstacle avoidance method based on double bispin Lyapunov Vector field. The method comprises the steps that the flight constraint condition of an unmanned aerial vehicle is determined, and an obstacle safety circle is constructed; obstacle avoidance decision is carried out through the obstacle safety circle; and the optimal obstacle avoidance direction and a vector field rotation direction are determined to carry out obstacle avoidance. In order to improve the obstacle avoidance efficiency and shorten an obstacle avoidance path, the criterionof successful obstacle avoidance is redefined. In order to simplify the complexity of obstacle avoidance, an obstacle merge reconfiguration rule for avoiding multiple tiny obstacles is provided. The method can meet the dynamic constraint of the unmanned aerial vehicle, realizes static and dynamic obstacle avoidance, and realizes autonomous obstacle avoidance of the unmanned aerial vehicle in a dynamic unknown environment.

Description

technical field [0001] The invention belongs to the control field of unmanned aerial vehicle space obstacle avoidance flight, mainly relates to the method of simultaneously satisfying the dynamic constraints of unmanned aerial vehicle and realizing static and dynamic obstacle avoidance, especially relates to a kind of unmanned aerial vehicle based on double-spin Lyapunov vector field Aircraft obstacle avoidance method. Background technique [0002] As a kind of aircraft that can be controlled autonomously or remotely, it has attracted more and more attention due to its high endurance and maneuverability, and its obstacle avoidance technology during flight has also become a research hotspot. [0003] At present, there are many researches on obstacle avoidance flight of unmanned aerial vehicles, and the existing obstacle avoidance algorithms can be mainly divided into three categories: heuristic algorithms, methods based on graph theory and geometric methods. Among them, the ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05D1/10
Inventor 张毅孟启源杨秀霞崔嘉华伟罗超曹唯一
Owner NAVAL AVIATION UNIV
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