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Anti-collision control method for UAV formation flight turning

A formation flight and control method technology, applied in the field of route planning, can solve problems such as increasing the probability of collision accidents, drone collisions, system instability, etc., and achieve the goal of solving anti-collision problems, avoiding damage, and reducing tracking errors Effect

Inactive Publication Date: 2017-02-22
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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Problems solved by technology

[0003] The formation maintenance of UAV formation flight is particularly important when turning. Most of the current route planning algorithms do not fully consider the maneuverability limitations of UAVs, especially the speed limit. If the flight speed cannot be reduced to the theoretical design value specified by the route, it will easily collide with the outside UAV, and when the formation transitions from straight flight to turning flight, due to the switching of the control law, it is easy to cause the system to malfunction. Stability, which in turn increases the probability of collision accidents when turning

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[0043] The present invention provides a UAV formation flying turning anti-collision control method. In order to make the object, technical solution and effect of the present invention clearer and clearer, the present invention will be further described in detail with reference to the accompanying drawings and examples. It should be understood that the specific implementations described here are only used to explain the present invention, not to limit the present invention.

[0044] Adopt the UAV formation flight turning anti-collision control method of the present invention, specifically follow the following steps.

[0045] Step 1. Calculate the maneuverability limit of the UAV, that is, the relative maximum and minimum speed. Considering that the actual speed control system is generally designed in the form of underdamping, and there is an overshoot in the tracking, so adding σ=20% overshoot to the limit of the actual maximum and minimum speed results in a relative maximum an...

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Abstract

The invention provides a turning anti-collision control method for UAV formation flight. Aimed at an isomorphic lead aircraft and wining plane type rhombus formation, a method based on airway restriction is used. According to maneuvering characteristic limitation of an UAV, the turning airway of the lead aircraft is corrected, and wining planes change respective airways according to the relation positions with the lead aircraft. Thus, a practical formation turning airway is generated. Using the anti-collision method, formation tacking error is reduced, and the method prevents the formation structure from being damaged. On airway planning, the method solves a problem of anticollision when the formation turns.

Description

technical field [0001] The invention relates to an anti-collision control method for UAV formation flight turning, in particular to a UAV formation turning route restriction method, which belongs to the field of route planning. Background technique [0002] In addition to the mobility and agility of UAVs, the development of modern UAVs also requires UAVs to have the ability of multi-machine cooperative flight and combat. UAV formation flight is to arrange multiple UAVs with autonomous functions in a three-dimensional space according to a certain structural form to ensure the stability of the formation during the flight process, but it can be dynamically adjusted according to changes in external conditions and mission requirements. . The success rate of UAV formation missions and the ability to resist emergencies are much higher than those of single flight, and the short-distance formation can effectively increase the aerodynamic performance of UAVs in the following position...

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05D1/10
Inventor 郜晨龚华军甄子洋郑峰婴
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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