Multi-UAV (unmanned aerial vehicle) dynamic formation control method

A control method and multi-UAV technology, applied in the field of flight control, can solve the problems of poor formation rigidity and the requirement to reduce the update rate of the formation wireless data link, etc.

Active Publication Date: 2012-07-18
BEIHANG UNIV
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AI Technical Summary

Problems solved by technology

[0008] The purpose of the present invention is to solve the problem of formation control of miniature unmanned aerial vehicles that is convenient for engineering, and propose a dynamic formation control method for multiple UAVs. The behavior-based formation control method reduces the requirement on the formation wireless data link update rate, and enhances the obstacle avoidance ability of the UAV swarm formation; in view of the shortcomings of the traditional behavior-based formation control method, the formation rigidity is not good, and a virtual The structure is used as a reference. Through the fusion of the two formation methods, the advantages of each method can be brought into play: under the premise of maintaining a relatively stable formation, the ability of micro-UAVs to avoid obstacles and threats in unknown environments can be enhanced. There is a certain reference value for the cooperative low-altitude penetration of aircraft groups

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Embodiment Construction

[0083] The present invention will be further described in detail below in conjunction with the accompanying drawings.

[0084] The dynamic formation control method of multiple drones proposed by the present invention includes the following steps:

[0085] Step 1: Formation maintenance method;

[0086] (1) Establish the ground coordinate system XOY;

[0087] Establish the ground coordinate system XOY, such as figure 1 As shown, the X axis represents the east position and the Y axis represents the north position. ML and MF represent the formation leader and wingman respectively, Ψ L And Ψ F Represents the track deflection angle of the leader and the wingman, respectively, MV represents the wingman set by the virtual structure, referred to as the virtual wingman, L and a represent the expected distance and observation angle of the virtual wingman to the leader, L l And a l They represent the distance and observation angle of the actual wingman to the lead aircraft. The existing communic...

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Abstract

The invention discloses a multi-UAV (unmanned aerial vehicle) dynamic formation control method, and belongs to the technical field of flight control. The multi-UAV dynamic formation control method includes steps as follows: step 1, a formation keeping method; step 2, an obstacle avoidance method; and step 3, a behavior-based formation process, wherein the behavior-based formation process includes behavior decomposition and control realization. The method solves the defect that the traditional virtual structure manner formation control has higher communication quality requirement; the behavior-based formation control method is introduced to lower the requirement of formation wireless data link update rate and enhances the obstacle avoidance capability of the UAV group formation; and aiming at the defect that the traditional behavior-based manner formation control cannot keep good formation rigidity, a virtual structure is introduced for reference. On the premise of keeping the relatively stable formation, the capability of obstacle and threat avoidance of a microminiature UAV can be enhanced, and the method has a certain reference value for UAV group cooperation low-altitude penetration.

Description

Technical field [0001] The invention relates to a micro-unmanned aerial vehicle formation control, belonging to the technical field of flight control, and in particular to a dynamic formation control method for multiple drones. Background technique [0002] At present, as many as 30 countries have invested a lot of human and financial resources in the research and production of drones. After two decades of development, this technology has been relatively mature and has played a role in various military and civilian fields. However, there are some problems when a single UAV performs missions. For example, a single UAV may be affected by the number of sensors. Restrictions, it is impossible to observe the target area from multiple angles and all directions. When facing a large-area search task, it cannot effectively cover the entire search area; if it is a rescue mission, a single UAV is restricted in terms of load, which is often affected The efficiency of the entire rescue will ...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/10
Inventor 吴森堂孙健胡楠希杜阳
Owner BEIHANG UNIV
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