Distributed fault-tolerant management method of multi-UAV formation structure

A distributed fault-tolerant, multi-UAV technology, applied in the field of UAV control and decision-making

Active Publication Date: 2016-02-24
HEFEI UNIV OF TECH
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  • Application Information

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Problems solved by technology

[0004] In order to overcome the shortcomings of the existing fault-tolerant management method of multi-UAV formation structure, the present invention proposes a distributed fault-tolerant management method of multi-UAV formation structure, in order to combine multiple UAV formations When the UAVs are damaged during the flight of the complex UAV formation, the remaining UAVs can make independent decisions to uniquely determine one of the UAVs to complete the adjustment of the formation structure, so as to ensure that the multi-unmanned The stability of the UAV formation structure improves the reliability and robustness of the fault-tolerant management of the multi-UAV formation structure

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Embodiment Construction

[0101] In order to make the technical solution of the present invention more clear and complete, further description will be made below in conjunction with the accompanying drawings and the specific implementation case of the distributed fault-tolerant management of the multi-UAV formation composed of m UAVs in the present invention.

[0102] refer to figure 1 , in this embodiment, a distributed fault-tolerant management method of a multi-UAV formation structure is applied in a flight control environment composed of m UAVs and a ground control center; in the flight control environment there is a The leading UAV leads other UAVs to fly towards the target according to the predetermined track; m UAVs are recorded as u={u 1 , u 2 ,...,u i ,...,u m}, 1≤i≤m; i represents the unique number of the UAV, u i Indicates the i-th UAV; the method proceeds as follows:

[0103] Step 1. The ground control center constructs the initial formation structure, and converts the initial formatio...

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Abstract

The present invention discloses a distributed fault-tolerant management method of a multi-UAV formation structure. The method is characterized by comprises the following steps that: (1) a ground control center builds an initial formation structure and sends the structure to all UAVs, (2) each of the UAVs autonomously form an initial formation structure together and flies, (3) each of the UAVs judges whether other UAVs is newly damaged or not, and the method returns to the step (3) if not, (4) the remaining UAVs judge whether need to be responsible to calculate the formation structure again or not, and a step (5) is executed if so, whether a new formation structure message is received or not is judged if not, a step (6) is executed if the new formation structure message is received, otherwise the remaining UAVs continue to wait, (5) the new formation structure is reconstructed and sent to other UAVs, and (6) the remaining UAVs autonomously form a new formation structure and fly, and the method returns to the step (3). According to the distributed fault-tolerant management method, the multi-UAV formation structure with multi-level composition can be supported, and the formation structure can be rapidly and autonomously reconstructed when the UAVs are damaged, and the reliability and robustness are high.

Description

technical field [0001] The invention relates to fault-tolerant management of multi-unmanned aerial vehicles formation structure, and belongs to the field of unmanned aerial vehicle control and decision-making. Background technique [0002] The fault-tolerant management of the multi-UAV formation structure refers to the use of the remaining UAVs in the formation to complete the formation structure when one or more UAVs in the formation are damaged during the execution of tasks in the multi-UAV formation. Adjust to maintain the stability of the formation structure, so as to ensure the smooth completion of formation tasks. [0003] The traditional fault-tolerant management method of multi-UAV formation structure is mainly centralized, and a master control center (which can be a ground control center or a central UAV) is required to track the status of the formation. When one or more UAVs are damaged, the main control center is responsible for controlling the remaining UAVs in ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/10
CPCG05D1/10
Inventor 杨善林王国强罗贺胡笑旋马华伟靳鹏夏维
Owner HEFEI UNIV OF TECH
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