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Unmanned aerial vehicle flight control method

A flight control and unmanned aerial vehicle technology, applied in the direction of non-electric variable control, control/adjustment system, three-dimensional position/channel control, etc., can solve the problem that it is difficult to achieve convergence, it is difficult to achieve intelligent control with high real-time, high precision, and inability to complete, etc. question

Pending Publication Date: 2020-01-24
SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP OF CHINA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The key to introducing artificial intelligence into the control of UAVs is to rationalize dimensionality reduction and build complex control models. UAVs in complex environments have hundreds of variables related to high-dynamic flight, reflecting the over-dimensionality of the flight scene control model. If there are too many dimensions, it is difficult to achieve convergence when training it, so that the training cannot be completed; if the number of dimensions is too small, the information of branch reduction is too much, and it is difficult to achieve the effect of intelligent control with high real-time and high precision

Method used

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  • Unmanned aerial vehicle flight control method
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  • Unmanned aerial vehicle flight control method

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Embodiment Construction

[0052] The application will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the related application, not to limit the application. In addition, it should be noted that, for ease of description, only parts relevant to the present application are shown in the drawings.

[0053] It should be noted that, in the case of no conflict, the embodiments in the present application and the features in the embodiments can be combined with each other. The present application will be described in detail below with reference to the accompanying drawings and embodiments.

[0054] It should be noted that in the description of this application, the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc. The terms of the indicated direction or positional relationship are based on the direction or positional ...

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Abstract

The invention belongs to the technical field of unmanned aerial vehicle flight control, and particularly relates to an unmanned aerial vehicle flight control method. The method comprises the steps of:setting a maneuvering mode of an unmanned aerial vehicle as a shooting interception maneuvering mode during long-distance engagement; setting the maneuvering mode of the unmanned aerial vehicle as anoffset maneuvering mode after ammunition is shot; setting the maneuvering mode of the unmanned aerial vehicle as a cross-cut maneuvering mode while elude the locking of the enemy; and setting the maneuvering mode of the unmanned aerial vehicle as an escape maneuvering mode, a cocking looping maneuvering mode or a breaking S maneuvering mode when eluding the attack of a guided missile.

Description

technical field [0001] The application belongs to the technical field of unmanned aerial vehicle flight control, and in particular relates to a method for controlling unmanned aerial vehicle flight. Background technique [0002] The introduction of artificial intelligence in UAV control can adapt to and respond to complex and changing environments, and automatically generate control behaviors, so as to get rid of human physiological and psychological limitations, without physical limits, and always maintain rapid and accurate responses. [0003] The key to introducing artificial intelligence into the control of UAVs is to rationalize dimensionality reduction and build complex control models. UAVs in complex environments have hundreds of variables related to high-dynamic flight, reflecting the over-dimensionality of the flight scene control model. If there are too many dimensions, it is difficult to achieve convergence when training it, so that the training cannot be complete...

Claims

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Application Information

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IPC IPC(8): G05D1/10
CPCG05D1/104
Inventor 孙智孝郎魁军朴海音马启兵李思凝李俊男骆遥杜冲刘仲葛俊杨芳王言伟张少卿
Owner SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP OF CHINA
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