Multi-airplane formation flight control method

A technology of formation flight and control method, applied in the direction of non-electric variable control, control/regulation system, three-dimensional position/course control, etc.

Active Publication Date: 2016-08-10
XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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Problems solved by technology

[0004] The purpose of the present invention is to provide a multi-machine formation flight control method to solve or at least alleviate at least one problem in the background technology

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  • Multi-airplane formation flight control method
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  • Multi-airplane formation flight control method

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[0022] In order to make the objectives, technical solutions and advantages of the present invention clearer, the technical solutions in the embodiments of the present invention will be described in more detail below in conjunction with the drawings in the embodiments of the present invention. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are some, but not all, embodiments of the invention. The embodiments described below by referring to the figures are exemplary and are intended to explain the present invention and should not be construed as limiting the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention. Embodiments of the present invention will be described in detail below ...

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Abstract

The invention discloses a multi-airplane formation flight control method comprising the following steps: in step S1, according to initial formation design, an initial formation matrix is constructed; in a step S2, in practical flying processes, a practical formation matrix is constructed; in step S3, a strategy set is determined according to airplane performance boundaries; in step S4, an error matrix is calculated, and an error matrix determinant is associated with a formation situation value; in step S3, according to the strategy set determined in step S3, each strategy is gone over, and a strategy corresponding to a maximum formation situation value is chosen and executed; in step S6, an instruction corresponding to the maximum situation value is transmitted to an automatic flight control system which can control a flying state of an airplane, and therefore target formation control can be fulfilled; in step S7, if disturbance occurs in a target formation and the formation situation value can reach a maximum state, then procedures from step S1 to step S6 are repeated. The beneficial effects of the multi-airplane formation flight control system are that when a problem of fixed formation flight control is solved, a problem of group formation flight control is also addressed, and a multi-airplane task execution success rate is improved.

Description

technical field [0001] The invention relates to the technical field of flight control, in particular to a multi-aircraft formation flight control method. Background technique [0002] The task of formation flight control is to control multiple aircraft to fly in the air according to a predetermined formation, and provide technical support for manned aircraft flight performances and unmanned aerial vehicle formation flight. [0003] With the increasing development of UAV technology, the demand for reconnaissance and strike combat missions based on multi-aircraft formations is becoming more and more obvious. A multi-aircraft cluster flight control method suitable for reconnaissance is required, and at the same time taking into account the need for concealment. The formation flight control method of multi-aircraft flying in tight formation to reduce the detection of enemy radar has become a major difficulty in research. Due to the limited shape, it is impossible to realize the...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/10
CPCG05D1/104
Inventor 张帅刘峰王鸿翔周涛何坤
Owner XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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