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Multi-unmanned plane formation flight path planning method based on hungarian algorithm

A Hungarian algorithm and multi-UAV technology, applied in the field of multi-UAV formation track planning based on the Hungarian algorithm, can solve the problems of long planning time, long design cycle, and easy stagnation

Inactive Publication Date: 2018-11-02
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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Problems solved by technology

The basic characteristics of the existing technology are that the model is relatively complex, the amount of calculation is large, the planning time is long, and it is easy to stagnate, and the formation design and track planning are basically carried out separately, and the design cycle is very long

Method used

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Embodiment Construction

[0035] The present invention will be described in detail below in combination with specific embodiments.

[0036] The steps of the multi-UAV formation track planning method based on the Hungarian algorithm of the present invention are as follows:

[0037] Step 1: Input the number of UAVs in the formation, the relative initial coordinates of the UAVs, and the final coordinates of the final UAVs to form the formation in the matlab software;

[0038] Step 2: Calculate the distance between the initial position of n drones and n target points to form an n*n distance matrix A;

[0039] In the UAV allocation problem, the row or column of the distance matrix is ​​changed so that there are zero elements in each row and column, and a zero-element matrix containing n different rows and different columns is finally obtained through the corresponding adjustment strategy. This results in full distribution with the shortest total distance the drone flies.

[0040] Step 3: Transform the dis...

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Abstract

The invention aims to provide a multi-unmanned plane formation flight path planning method based on a hungarian algorithm. The distance between the initial position of the unmanned aerial vehicle andthe target point forms a distance matrix. The distance matrix is transformed, zero elements are selected to be marked, and the number of the zero elements is counted, whether the optimal solution of the assignment problem is met or not is judged, and the zero element in the matrix is covered with the minimum. The minimum value among all elements without the minimum coverage is found out, and the value from all uncovered elements is subtracted, and the elements in all the marked columns are added with the value, so that the position of the original zero element is not changed. A result matrix corresponding to the optimal solution can be obtained by repeatedly executing the above steps. Transformation is carried out to obtain the optimal solution, and after the distribution is finished, thesimulation flight is carried out, so that whether the collision exists or not is judged, and otherwise, the obstacle avoidance is needed. The method has the advantages of being high in practicability,simple in model and small in calculation amount, short in time of formation design and flight path planning, and is high in efficiency.

Description

technical field [0001] The invention belongs to the technical field of unmanned aerial vehicles, and relates to a multi-unmanned aerial vehicle formation track planning method based on the Hungarian algorithm. Background technique [0002] With the development of modern science and technology and the continuous increase of military and political needs, in many cases a single UAV can no longer meet the mission requirements, so multi-UAV formation technology has become a research hotspot. At the same time, for civilian use, UAV formation flight performances have also been a hot topic in recent years. The number of UAVs flying in formation has grown from a few dozen at the beginning to thousands now. The key technical issues of UAV formation flight mainly include formation design, aerodynamic coupling, formation dynamic adjustment, track planning and formation flight control strategy, etc. The Hungarian algorithm is a combinatorial optimization algorithm used to solve assignme...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/10
CPCG05D1/104
Inventor 盛汉霖叶勇杰李嘉诚张杰黄伟陈芊
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS